Writing about aerospace and electronic systems, particularly with defense applications. Areas of interest include radar, sonar, space, satellites, unmanned plaforms, hypersonic platforms, and artificial intelligence.
IEEE Spectrum · Aerospace · Signal Processing · April 2026
Radar Imaging
For seventy years, the region straight ahead of a
moving aircraft has been radar's worst neighborhood. A new class of
space-time super-resolution algorithms — now fast enough for real-time
flight — is finally changing that.
By Stephen L Pendergast, Senior Life Member, IEEE · 23 April 2026
BLUF
A team at Nanjing University of Aeronautics and Astronautics has
published a method that cuts the computational cost of multichannel
forward-looking radar super-resolution by roughly three orders of
magnitude, from O(M³N³) down to O(r³),
without giving up resolution. The approach — Doppler-domain
dimensionality reduction combined with covariance-matrix rank reduction —
closes one of the last practical barriers to fielding super-resolution
imaging on aircraft, missiles, rotorcraft, and, eventually, automobiles.
Measured X-band airborne data shows a better than 3× speedup over the
baseline space-time algorithm and roughly 20× over conventional
full-dimensional processing, while image entropy and contrast hold
within a few percent of the unaccelerated reference. The result has
implications well beyond the laboratory: brownout landing aids, missile
terminal seekers, autonomous-vehicle imaging radar, and the "blind
landing" problem that has plagued military rotorcraft for two decades
all share the same underlying mathematics.
The airspace directly in front of a moving radar platform is a
cursed place. It is also the one place a pilot most wants to see. When
an airliner descends through fog toward a runway, when an attack
helicopter flares into a dust cloud of its own making, when a missile
commits to its final mile, or when an autonomous truck enters a blizzard
— the sensor must interrogate the sector straight ahead. And that is
precisely the geometry in which radar performs worst.
The reason is geometric and unforgiving. Synthetic-aperture radar
(SAR), the workhorse of high-resolution imaging, gets its remarkable
cross-range resolution from the Doppler spread that accumulates as the
platform flies past a target. Look sideways and the Doppler
signature varies richly across the scene; look forward and the variation
collapses toward zero. Worse, targets that are mirror-symmetric about
the flight axis produce identical Doppler returns, so the radar cannot
tell left from right by spectrum alone. Doppler beam sharpening, the
simpler cousin of SAR that powered the first terrain-following attack
radars in the 1960s, fails for the same reason.
So forward-looking radar has traditionally settled for what the
antenna can give it. A real-aperture radar with a one-meter dish at
X-band produces an azimuth beam roughly two degrees wide. At 70 km — a
typical standoff for an airborne surveillance sortie — that beam smears
the ground into a lateral blur more than two kilometers across. No
amount of averaging fixes that; the information is never collected.
The super-resolution detour
The response from the signal-processing community, building over
the last quarter century, has been to extract resolution from
mathematics rather than aperture. The field of array signal processing
offered a starting toolkit — MUSIC, ESPRIT, the Iterative Adaptive
Approach (IAA), Sparse Iterative Covariance-based Estimation (SPICE),
Sparse Asymptotic Minimum Variance (SAMV), and Sparse Bayesian Learning
(SBL), among others — originally developed for direction-of-arrival
estimation in passive sonar and radio astronomy.3,4
Applied to forward-looking radar, these estimators can resolve targets
separated by a fraction of the physical beamwidth, provided the
measurement model is clean and the signal-to-noise ratio is high.
The German Aerospace Center (DLR) demonstrated one of the earliest
hardware incarnations in the late 1990s with SIREV — the Sector Imaging
Radar for Enhanced Vision — a helicopter-mounted forward-looking system
using a linear receive array and an extended chirp-scaling processor.5,6
SIREV established the basic architecture that most modern work still
follows: a multichannel receiver oriented perpendicular to the flight
axis, coherent processing that combines the spatial degrees of freedom
of the array with whatever limited Doppler information is available, and
image reconstruction that does not wait for the aircraft to fly past
its target.
The U.S. Army Research Laboratory pursued a parallel thread with
the Synchronous Impulse Reconstruction (SIRE) forward-looking
ground-penetrating radar, aimed at buried-explosive detection.7
And in rotorcraft, the Army's Degraded Visual Environment Mitigation
(DVE-M) program — later called BORES — folded 94-GHz millimeter-wave
radar into fused sensor suites designed to guide helicopters onto
landing zones obscured by dust and snow.8,9
The Army attributes roughly three-quarters of its rotorcraft accidents
in Iraq and Afghanistan to brownout, and DVE-induced spatial
disorientation remains a leading cause of fatal civilian helicopter
crashes.9,10
But all of these efforts ran into the same computational wall.
Super-resolution algorithms work by repeatedly forming, inverting, and
updating a covariance matrix whose size grows as the product of the
number of spatial channels M and the number of coherent pulses N′.
A modern multichannel system with eight channels and a few hundred
pulses per dwell produces covariance matrices with tens of thousands of
rows. Inverting them naïvely costs O(M³N′³) floating-point operations per iteration. The math works. The silicon does not — at least not at video rates on an airframe.
An end-run around the matrix
Lingyun Ren, Di Wu, Daiyin Zhu, and colleagues at Nanjing
University of Aeronautics and Astronautics' Key Laboratory of Radar
Imaging and Microwave Photonics laid out a candidate space-time
framework — Space-Time Reiterative Super-Resolution, or ST-SR — in 2024.11 It used a robust iterative super-resolution engine to exploit spatial and
slow-time degrees of freedom jointly, and it did produce dramatically
sharper forward-looking imagery than spatial-only processing. It was
also, the authors concede, too slow to fly.
Their April 2026 paper in IEEE Transactions on Geoscience and Remote Sensing is the sequel that fixes the speed problem.1 The core observation is unromantic but powerful: in forward-looking geometry, the Doppler spectrum is nearly empty.
The high Doppler centroid and compressed bandwidth that make
forward-looking imaging hard in the first place also guarantee that the
scene energy occupies only a small fraction of the available Doppler
bins. Everything else is redundancy.
"The computational complexity is reduced from
O(M³N³) to O(r³), where r is much smaller than MN — while maintaining
imaging fidelity."
The Nanjing team exploits that redundancy in two cascaded steps.
First, after compensating for the range-varying Doppler centroid, they
transform the received data cube to the Doppler domain and keep only
those bins that hold roughly 90 to 100 percent of the total signal
energy. For a typical scene this knocks the working dimension from
hundreds of pulses down to a handful of dozens. Second, they perform a
partial singular-value decomposition of the resulting space-time
covariance matrix and retain only the first r
eigenvectors — the dominant signal subspace. The noise subspace, which
contributes nothing useful to azimuth estimation, is discarded.
The effect on the inner loop is dramatic. In their published
benchmarks, surface-scene imaging that took 400 seconds under
conventional ST-SR completes in about 20 seconds after dimensionality
and rank reduction — a better than 20× speedup on an Intel Xeon Platinum
8168. Image entropy and contrast move by less than three percent.
Measured X-band airborne data processed at r = 6 yielded a 3× speedup over baseline ST-SR, while showing visibly cleaner clutter suppression than the full-dimension algorithm.1
How the acceleration works
A multichannel radar collects an L × N′ × M data cube (range gates ×
pulses × channels). The conventional space-time super-resolution method
forms a covariance matrix of size N′M × N′M and inverts it every
iteration. The new method first projects the data onto the K′ most
energetic Doppler bins (with K′ ≪ N′), then keeps only the r largest
eigenvectors of the reduced covariance (with r ≪ K′M). The matrix that
actually gets inverted is r × r — often as small as 6 × 6 or 8 × 8. That
is where the three-orders-of-magnitude speedup lives.
The navigation problem
A second contribution in the paper is less headline-grabbing but
arguably more consequential for operational deployment: the algorithm no
longer depends on the inertial navigation system (INS) to tell it how
fast the aircraft is moving or at what elevation angle each range cell
is observed. Instead, it pulls those parameters directly out of the
range-Doppler image itself, by tracking the sharp spectral edge that
marks the baseband Doppler centroid of the forward-looking region.
This matters because INS errors are the silent killer of coherent
super-resolution. A velocity estimate off by one percent, or a heading
drift of half a degree, is enough to smear a super-resolution image into
an ordinary real-beam one. Pulling motion parameters from the radar
echoes themselves — what DLR's SIREV team called "extracting motion
errors from the range-compressed raw data"6
— is a standard technique in SAR autofocus, but in forward-looking
multichannel work it has been rare. The Nanjing method does it cheaply:
the Doppler edge is robust down to roughly a –5-dB signal-to-clutter
ratio in the authors' Sea State 6 simulations, which is encouraging for
operation in heavy sea clutter or over vegetated terrain.
Why this is not just a Chinese radar-imaging paper
The algorithm was developed for airborne surveillance radar. Its implications sprawl much wider.
In helicopter brownout mitigation, the U.S. Army's
DVE-M program has spent more than a decade fusing lidar, long-wave
infrared, and millimeter-wave radar into synthetic-vision helmets for
UH-60 and CH-47 crews.9,10
Lidar fails in fog; IR struggles in heavy dust. Millimeter-wave radar
penetrates both, but the short aperture mounted on a helicopter nose
delivers poor azimuth resolution without super-resolution processing.
Forward-looking SAR concepts proposed at the Army Research Laboratory
have pursued exactly this path — a linear receive array plus signal
processing to extract the third dimension from small pitch variations
during approach.12 A computationally tractable space-time algorithm is precisely what such a system would need.
In missile terminal guidance, the trend across
active radar homing (ARH) seekers — from Lockheed Martin's LRASM to the
ESSM Block 2 to the SM-2 Block IIICU — is toward richer onboard imagery
for target discrimination against decoys and clutter in dense
electromagnetic environments.13,14
The engagement geometry is pure forward-looking: the seeker is racing
toward the target. Every gain in azimuth resolution is a gain in the
probability of picking the right ship out of a convoy, or the right
vehicle out of a column. A O(r³) super-resolution kernel is the kind of workload that can plausibly run on a rad-hardened embedded processor inside a missile.
In automotive imaging radar, the 4D MIMO boom —
Continental's ARS540, Arbe Robotics' Phoenix with 1,728 virtual
channels, Uhnder's S81 using digital code modulation — is pushing
angular resolution toward LiDAR-like performance while keeping radar's
all-weather penetration.15,16,17
Market research firms project the 4D imaging radar segment growing from
roughly USD 2 billion in 2024 to USD 10 billion by 2030, a compound
annual growth rate near 38 percent.15
Every one of those chips faces the forward-looking geometry (a car
mostly cares about what is in front of it) and every one of them has to
run super-resolution at frame rates on a few watts. The Nanjing team's
Doppler-sparsity exploitation and rank-reduction tricks are directly
relevant to that embedded-automotive problem, even if the paper's
authors do not say so.
In autonomous-vehicle and robotic platforms, a
similar forward-looking MIMO-SAR concept has been explored by Belgian
and European researchers who explicitly cite DLR's SIREV work as
inspiration, combining forward-looking SAR with MIMO diversity to
sharpen angular resolution for ground robots.18 Here, too, the computational envelope is the binding constraint.
What is still missing
The Nanjing work leaves several questions open. The measured-data
validation uses an X-band airborne system with four receive channels and
a 500-Hz pulse-repetition frequency — a relatively benign configuration
compared with the hundreds of virtual channels in modern automotive
chips or the Ku- and Ka-band seekers in many missile terminals. The
authors' complexity analysis scales favorably, but real silicon
implementations will stress memory bandwidth at least as much as raw
FLOP count.
The algorithm also assumes a well-behaved sample covariance. In
scenarios with strong discrete scatterers — ships on open water,
powerlines against flat terrain, or vehicles in a parking lot — the
eigenvalue spectrum may not fall off as cleanly as in the measured data
the authors show. Truncating to too small an r
would then bleed strong targets into the noise floor. The paper's Sea
State 6 K-distribution simulations address this in part; broader clutter
benchmarks will have to come from independent groups.
And the whole family of covariance-based super-resolution methods
still carries a philosophical vulnerability: they resolve targets the
model predicts. Off-grid targets, scatterers with motion independent of
the platform, and adversarial jammers designed to exploit the sparsity
assumption can all produce artifacts that look like real objects. This
is not a flaw unique to the Nanjing work — it afflicts IAA, MUSIC, SBL,
and every other member of the family — but operational deployment will
require calibration, validation, and honest documentation of failure
modes that academic papers rarely provide.
A seventy-year-old problem, nearly solved
Radar engineers have been trying to see straight ahead since the
Normandy invasion, when H2S sets aboard RAF Pathfinders mapped
coastlines from abeam but went blind toward the aircraft's nose. The
intervening decades produced a tower of clever partial solutions:
monopulse for accurate single-target tracking, DBS for off-axis mapping,
bistatic SAR for forward-looking synthetic aperture at the cost of
doubled hardware. None of them gave a moving platform a genuinely sharp
picture of what lay directly in its path.
Combining the space-time model with aggressive, geometry-aware
dimensionality reduction may finally tip that balance. If the
performance numbers from the Nanjing group hold up in independent
benchmarks — and if embedded implementations match them on
airframe-grade hardware — the forward blind spot that has shaped radar
doctrine since the Second World War will become just another region of
the sky, no harder to image than any other. That would be a quiet
revolution. Those are usually the consequential kind.
References
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D. Zhu, "An Efficient Space-Time Forward-Looking Imaging Method for
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Reconstruction (SIRE) Forward-Looking Radar," Proc. SPIE 6561, Unmanned Systems Technology IX, April 2007. doi:10.1117/12.723688.
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in 'brownout' conditions," Yuma Proving Ground public affairs, 18 Oct.
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The Secretary of the Navy was fired by social-media
post while his ships were enforcing a blockade. The replacement for the
destroyer we couldn't build is now a battleship we can't afford. And the
carrier we have is being reviewed by the administration that owns it.
Admiral Zumwalt would not recognize this Navy — and he would not be kind
to those who built it.
By Pseudo Publius · Contributor
Bottom Line Up Front
On 22 April 2026, Defense Secretary Pete Hegseth fired Secretary of
the Navy John C. Phelan by public announcement from the Pentagon's chief
spokesman while Phelan was on Capitol Hill briefing Congress on the
Navy's budget. The firing came one day after Phelan, at the Navy
League's Sea-Air-Space symposium, publicly defended the proposed
Trump-class Guided Missile Battleship (BBG[X]) — a three-ship program
with a lead-ship cost of $17.47 billion and a program-of-record cost of
$43.5 billion — and announced that the Navy is reviewing the Ford-class
carriers CVN-82 and CVN-83 for possible redesign or cancellation. The
acting Secretary, Under Secretary Hung Cao, was sworn into his
number-two position only six months ago and has no prior shipbuilding
portfolio. The precipitating dispute was not policy; it was that Phelan
could not deliver the President's 2028 battleship keel-laying on a
schedule the industrial base cannot physically meet — the published plan
slips delivery to August 2036 — and that Phelan's direct texting
relationship with the President had come to irritate the Secretary of
Defense. Meanwhile, the Fiscal Year 2027 budget request asks for $65.8
billion for Navy shipbuilding while the Navy simultaneously reviews
whether to cancel two aircraft carriers that would sustain the statutory
11-CVN floor. The Zumwalt class — three hulls, roughly $25 billion sunk
— remains in search of a mission. Gerald R. Ford is on day 296
of deployment with fire-damaged berthing and a sewage system that fails
daily. This is not a coherent maritime strategy. It is improvisation at
the top of a Navy that has a war on, and the Sailors are absorbing the
consequences.
On the morning of Wednesday, 22 April 2026, the
Secretary of the Navy was on Capitol Hill discussing the service's
budget proposal with members of Congress. That afternoon, without
warning to him, the Pentagon's chief spokesman posted on X that
Secretary of the Navy John C. Phelan was "departing the administration,
effective immediately." Phelan, according to multiple accounts, learned
of his own firing from the post. He went to the White House in person
looking for the President. He could not find him. He walked the grounds
of the Eisenhower Executive Office Building asking anyone he recognized
whether the President actually knew. Eventually the President telephoned
him to confirm it. The next day, on Truth Social, the President called
Phelan "a long time friend, and very successful businessman" and said he
hoped to have him back in the administration someday. The Secretary of
War thanked him for his service and wished him well.
This happened while the United States Navy was enforcing a blockade
of Iranian ports. It happened during the Navy League's Sea-Air-Space
symposium — the service's single largest annual professional gathering —
at which Phelan had been the keynote speaker twenty-four hours earlier.
It happened two weeks after Hegseth removed the Army Chief of Staff,
the head of Army Transformation and Training Command, and the Army's
Chief of Chaplains. It is the first firing of a service secretary during
this administration, and the first firing of a sitting Secretary of the
Navy in wartime in living memory.
The firing was not, at bottom, about policy. Multiple accounts from the Washington Post, New York Times,
CNN, Axios, and NBC News converge on a set of proximate causes: Hegseth
believed Phelan was moving too slowly on shipbuilding reform; Hegseth
and Deputy Secretary of War Stephen Feinberg wanted shipbuilding
authority moved from the Navy Secretariat to the Office of the Secretary
of War; Phelan had a direct texting relationship with the President,
whose Mar-a-Lago residence is near Phelan's own Palm Beach mansion, and
the two reportedly exchanged late-night messages about "rusty ships."
Hegseth considered this an end-run around the chain of command. In a
White House meeting on shipbuilding Wednesday morning, the President
grew frustrated with slow progress and told Hegseth to "take care of
it." Hegseth did. The New York Times reported that Phelan had originally sold the President on the battleship program by showing him oil paintings of the Iowa-class
in action. He then spent thirteen months discovering that the U.S.
shipbuilding industrial base physically cannot deliver a
forty-thousand-ton capital ship on campaign-promise timelines. That
discovery cost him his job.
The Battleship That Cannot Be Built on Time
The specific shipbuilding program at the center of this dispute is the Trump-class
Guided Missile Battleship, designated BBG(X). Announced by the
President at Mar-a-Lago in December 2025 as the centerpiece of a new
"Golden Fleet," the class is envisioned as three large surface
combatants, 840–880 feet long and 35,000–41,000 tons displacement,
carrying deep vertical-launch magazines, Conventional Prompt Strike
hypersonic missiles, directed-energy weapons, and a revived
naval-gunfire capability of unspecified caliber. The lead ship is
notionally named Defiant.
The program's cost and schedule, as published by the Navy on the eve of Phelan's firing, are as follows:
BBG(X) Trump-class — FY 2027 Budget Submission
FY27 advance procurement funding$1.00 B
FY28 procurement (BBG-1 Defiant, net)$16.47 B
BBG-1 gross weapon-system cost$17.47 B
BBG-2 procurement (FY30, projected)$13.00 B
BBG-3 procurement (FY31, projected)$11.50 B
Program total across FYDP$43.50 B
Lead-ship award April 2028
Construction start August 2028
BBG-1 delivery August 2036
Several features of this table deserve attention. The first is that
$17.47 billion for a single surface combatant exceeds the projected
procurement cost of a follow-on Ford-class aircraft carrier, which the
Congressional Research Service places between $13 and $15 billion. The
Navy is proposing to pay more for one battleship than for one
nuclear-powered supercarrier. The second is that the delivery date —
August 2036 — is eight years after the President's original public
timeline. The third is that as of the FY27 budget submission, the Navy
had engaged exactly two vendors in concept conversations. No design had
been selected. No contract had been awarded. The acquisition strategy,
in Phelan's own Sea-Air-Space remarks, was still being worked out. On
those facts, the probability of laying Defiant's keel in 2028, as the President demanded, is not low. It is zero.
Phelan, to his credit, seems to have understood this. In his
Tuesday roundtable he acknowledged that the $17 billion figure "is the
early initial estimate" and said "we'll see where we really settle down
as we get through that and start to rationalize some of the costs." This
was the careful language of a financier who had run the numbers and did
not like what he saw. In the same session he defended the ship against
critics — "I've heard the critiques, too vulnerable, too expensive, too
big. We've heard that before about carriers and about submarines" — but
his defense was performative. The arithmetic had already defeated him.
He was fired twenty-eight hours later.
On those facts, the probability of laying Defiant's keel in 2028 is not low. It is zero.
The battleship's operational concept, as described in the FY27
budget justification and Phelan's own remarks, is worth reading
carefully. It is supposed to "deliver high-volume, long-range offensive
fires," serve as "a robust, survivable forward command and control
platform," host an embarked fleet staff, mount high-energy lasers and
electromagnetic railguns (neither currently fielded), reduce reliance on
expensive single-use munitions, and perform strike, air defense,
anti-submarine, and anti-surface warfare at the highest level. It is, in
other words, a battleship, a strike cruiser, a missile cruiser, a
command ship, a directed-energy testbed, and — if the railgun ever works
— a naval-gunfire platform, combined in one $17 billion hull. This is
the program management profile of the original Zumwalt class at conception. The reader is invited to recall how that turned out.
The Carrier That Is Under Review by the Administration That Owns It
On the same day Phelan rolled out the battleship budget, he also
disclosed that the Navy is conducting a formal review of the Ford-class
aircraft carriers CVN-82 (William J. Clinton) and CVN-83 (George W. Bush),
neither yet under contract. The stated purpose of the review is to
"review the costs, the designs, the systems, to make sure they make
sense, and they have all the systems and requirements that we want going
forward." The review is due to complete at the end of May 2026. Inside
Defense reported that senior Navy leadership has not ruled out
cancellation of future Ford-class hulls or a transition to a new design.
Phelan was notably candid about the specific subject of the review.
The Navy will evaluate, he said, "is the sortie rate generation that
much greater? And then, what are the cost implications of this electric
catapult? And did it really generate the savings? You know, the Navy
would like to say, 'we've saved five billion dollars in terms of savings
in number of men and maintenance.' I just need to check that back up."
That language — "I just need to check that back up" — is not the
language of a service secretary endorsing his own platform. It is the
language of a man conducting due diligence on a purchase someone else
made.
The background here matters. The President has repeatedly and
publicly disparaged the Electromagnetic Aircraft Launch System, insisted
the Navy should return to steam catapults, and described EMALS as
complicated nonsense. The Director of Operational Test and Evaluation's
FY2024 annual report — the most recent unclassified edition — states
that "the reliability and maintainability of CVN 78's EMALS and AAG
continue to adversely affect sortie generation and flight operations,
which remains the greatest risk to demonstrating operational
effectiveness and suitability" in Initial Operational Test and
Evaluation. Nearly nine years after commissioning, Gerald R. Ford's sortie-generation-rate testing has not been completed. The core performance claim of the class is unvalidated.
Whether a full redesign, an improved-Nimitz fallback, or a CVN-X
clean-sheet successor would serve the Navy better is a legitimate
question worth asking. It is not, however, a question one asks for the
first time while simultaneously asking Congress to fund a $43.5 billion
battleship program. A Navy that cannot decide whether it wants more
Ford-class carriers should not be ordering new classes of capital ships.
An Acting Secretary, a Blockade, and No Plan
Acting Secretary of the Navy Hung Cao brings a genuine Navy résumé
that his predecessor lacked. Born in Saigon, arriving in the United
States as a four-year-old refugee in 1975, Thomas Jefferson High School
for Science and Technology in the inaugural graduating class, Naval
Academy class of 1996 in ocean engineering, Naval Postgraduate School
for applied physics, a thirty-two-year career as a surface warfare
officer, explosive-ordnance-disposal officer, and deep-sea diver, with
combat deployments to Iraq, Afghanistan, and Somalia, retiring as a
captain in 2021. He led the recovery of John F. Kennedy Jr.'s aircraft
off Martha's Vineyard in 1999. He commanded the Naval Diving and Salvage
Training Center in Panama City. He later joined CACI International —
the same defense contractor that employed this writer for a portion of
his career — before two unsuccessful Republican runs for federal office
in Virginia.
Cao was confirmed as Under Secretary six months ago, on 3 October
2025, by a 52–45 Senate vote on party lines. Multiple accounts describe
his relationship with Phelan as strained. He has no shipbuilding
portfolio, no history as a carrier community advocate, no prior
engagement with the Ford-class review, and no established relationship
with either the Secretary of War or the President. He inherits, as of 22
April, a Navy conducting a blockade in the Strait of Hormuz, a carrier
on its 296th day at sea, a Ford-class design review due in four weeks, a
$43.5 billion battleship program his predecessor could not defend at
the speed the White House demands, a December 2025 Government
Accountability Office report on shipyard fire-safety oversight with six
unimplemented recommendations, and a fleet that has just suffered three
non-combat fires in six weeks. He also inherits whatever institutional
memory his predecessor took out the door with him.
The question not being asked in Washington this week is the one
that matters. It is not whether Hung Cao is qualified. It is whether the
civilian oversight architecture of the United States Navy — Service
Secretary, Under Secretary, five-star combatant commander relationships,
the testimony-before-Congress rhythm, the annual budget cycle — can
function when the Service Secretary is fired by social-media post for
failing to deliver a campaign promise that was physically impossible to
begin with. The answer, on present evidence, is no. It cannot.
What Admiral Zumwalt Would See
Elmo Russell Zumwalt, Jr., took the oath as the nineteenth Chief of
Naval Operations on 1 July 1970, at age forty-nine, the youngest in the
Navy's history. He inherited a service in crisis. Re-enlistment rates
after first hitch had collapsed to 9.5 percent against a target of 35.
The fleet was worn out by Vietnam. Race riots had erupted aboard Kitty Hawk and Constellation.
Morale was, in his own phrase, abysmal. Fourteen days into the job, he
sent a message to the entire fleet: "No other problem concerns me as
deeply as reversing the downward trend of Navy retention rates and I am
committing myself to improving the quality of Navy life in all respects
and restoring the fun and zest of going to sea." Over the next four
years he issued one hundred twenty-one Z-grams. Eighty-seven were
subsequently absorbed into the standing Navy directives system. He
integrated the Navy — "there is no black Navy, no white Navy; just one
Navy, the United States Navy" — appointed the first African-American
admiral, opened ships to women, eliminated what he called "Mickey Mouse"
regulations, authorized beards and civilian clothes aboard ship,
mandated thirty days' leave after deployment for at least half the crew,
and ordered that no Sailor should ever wait in line more than fifteen
minutes for anything. He diverted, by back-room arrangement, $40 million
from the equipment budget to servicemen's housing.
He did this during an active war. He did it with a smaller defense
budget than today's Navy enjoys in real terms. He did it because he
understood — as a destroyer skipper who had served in Robinson
at Leyte Gulf, as a brown-water commander in Vietnam, as a man whose own
son he watched die of cancer contracted from Agent Orange sprayed under
his own command — that the Navy's people are the Navy. Everything else
is hardware that floats.
"The Navy must instill at all levels an attitude which clearly recognizes the dignity and worth of each individual."
— Admiral Elmo R. Zumwalt, Jr., Z-gram 66, 17 December 1970
Set that record next to today's. A carrier crew improvising
sleeping quarters on mess-deck tables after their laundry caught fire.
Sailors working nineteen-hour watch cycles fishing T-shirts out of
undersized sewage pipes a contractor refused to redesign and the Navy
declined to insist on. A Sailor's mother photographing raw sewage
overflowing onto a berthing deck and contacting a public-radio reporter
because she could get no answer from the Navy. A Chief of Naval
Operations telling a Washington think tank that his Sailors "signed up
for this." A Secretary of the Navy pitching oil paintings of Iowa-class
battleships to a President whose attention span is measured in news
cycles, then being fired by X post because he could not deliver a $17
billion ship in two years. An acting Secretary sworn in during a
blockade with no confirmed successor on the Senate calendar. A $43.5
billion battleship program that no one outside the White House appears
to believe in. A Ford-class review that reads, on its face, like the
opening move of buyer's remorse.
Admiral Zumwalt did not agree with every decision his Navy made. He
was relieved and dismayed, in retirement, by what he regarded as the
erosion of material readiness and the drift of the surface force. He
would recognize some things about the 2026 Navy immediately: the strain
of extended deployments, the tension between the demands of combatant
commanders and the finite supply of hulls, the difficulty of retention
in a tight labor market. He would recognize those as old problems.
He would not recognize the rest. He would not recognize a Navy that
permits a Sailor's mother to be the person who breaks the news of a
habitability crisis. He would not recognize a civilian leadership that
fires its own Secretary by public announcement during wartime because he
could not deliver an impossible schedule fast enough. He would not
recognize an acquisition system that greenlights a $43.5 billion
battleship program built around directed-energy weapons and railguns
that do not yet work, while the lead ship of the class named for him
sits at Ingalls undergoing its third attempt at finding a mission. He
would not recognize a Navy in which the Secretary of the Navy, the Under
Secretary, the Chief of Naval Operations, and the President disagree in
public about whether the most expensive warship in the fleet actually
works, while that ship is deployed in combat operations against Iran.
He would call this, and he would be right, unserious.
Three Questions for the Acting Secretary
Acting Secretary Cao inherits a mess that is not of his making. He
also inherits, for as long as the administration leaves him in place,
the one job in the American defense establishment whose statutory
purpose is to act as the civilian conscience of the United States Navy.
Three questions are worth his early attention:
First: what is the maritime strategy the Golden Fleet is supposed to execute?
The BBG(X) budget documents assert that the battleship will "anchor the
high end of the Golden Fleet high-low mix" and operate as part of
"Battleship Strike Groups." No published document articulates what a
Battleship Strike Group is for that a Carrier Strike Group or a Surface
Action Group is not already for. Before Congress is asked to appropriate
$17 billion for Defiant, the service owes the country a
strategy paper. Project SIXTY, Admiral Zumwalt's September 1970
strategic assessment, was drafted in seventy-two days. The Golden Fleet,
sixteen months after its announcement, still lacks one.
Second: if the Ford-class review concludes that CVN-82 and
CVN-83 should not be ordered as currently configured, what does the Navy
propose instead? An improved Nimitz-class hull is feasible;
the basic design is proven, Newport News Shipbuilding retains the
tooling, and the EMALS/AAG retrofit risk disappears. A CVN-X clean-sheet
design is also feasible but adds a decade. Under no circumstance should
the Navy allow a gap to develop between Doris Miller's delivery and the next carrier order. The statutory 11-CVN floor is not an aspirational goal. It is U.S. Code.
Third: what is the acting Secretary's plan to address the conditions reported aboard Gerald R. Ford?
Not in the abstract. Specifically: the Vacuum Collection, Holding and
Transfer system redesign for CVN-79 before delivery in 2027; the
laundry-space fire suppression and berthing-ventilation isolation
retrofit for the deployed fleet; the implementation timeline for all six
GAO-26-107716 contractor-oversight recommendations; and the independent
habitability review this writer called for three days ago in these
pages. The Sailors did not fail the Navy. The Navy, at the top, is
failing them.
❦ ❦ ❦
A correspondent known to this writer, a retired senior engineer and
Navy veteran who served as an Engineering Duty Officer during Admiral
Zumwalt's tenure, put the matter plainly when these events were
described to him: "I don't think he would be proud of today's Navy." He
is not wrong. But Admiral Zumwalt's last, best lesson was not that
institutions inevitably decline. It was that they can be turned around.
He did it once, in a worse environment than this one, with fewer tools
and a larger problem. What he did required three things: a clear
strategy, an unflinching honesty about institutional failure, and an
absolute, non-negotiable commitment to the dignity and welfare of the
Sailors who do the actual work. The United States Navy in April 2026 is
short of all three. The Sailors are still there, doing their job. They
deserve, at minimum, civilian leadership willing to do the same.
Sources
All URLs verified as of 23 April 2026. Sources are listed in order of first reference.
Jaffe, Greg, Maggie Haberman, and Adam Entous. "Trump's Dreams for a Battleship Led to His Navy Secretary's Ouster." The New York Times, 23 April 2026.
Goldstein, Richard. "Elmo R. Zumwalt Jr., Admiral Who Modernized the Navy, Is Dead at 79." The New York Times, 3 January 2000.
U.S. Government Accountability Office. Navy Ship Maintenance: Fire Prevention Improvements Hinge on Stronger Contractor Oversight. GAO-26-107716, 17 December 2025. https://www.gao.gov/products/gao-26-107716
In the span of six weeks, fires struck three U.S. Navy
capital ships and displaced hundreds of Sailors. The pattern is not bad
luck. It is the predictable cost of a decade of concurrency, deferred
testing, and eroded oversight — and the Sailors are paying for it.
By Pseudo Publius · Contributor
Bottom Line Up Front
Between 12 March and 19 April 2026, three U.S. Navy combatants suffered non-combat fires: the carrier Gerald R. Ford (CVN-78) in the Red Sea, the carrier Dwight D. Eisenhower (CVN-69) in Norfolk Naval Shipyard, and the destroyer Zumwalt (DDG-1000) at Ingalls Shipbuilding in Pascagoula. The Ford
fire alone displaced more than 600 Sailors, burned for over 30 hours,
destroyed more than 100 berths, and forced the Navy to strip 1,000
mattresses from the not-yet-commissioned John F. Kennedy
(CVN-79). These events do not stand in isolation. They sit atop a
documented record of Vacuum Collection, Holding and Transfer (VCHT)
sanitation failures on Ford; unresolved reliability shortfalls
in the Electromagnetic Aircraft Launch System (EMALS) and Advanced
Arresting Gear (AAG); a Zumwalt-class program that consumed roughly $25
billion to field three ships now undergoing a second identity change;
and a December 2025 Government Accountability Office finding
(GAO-26-107716) that the Navy's shipyard fire-safety regime is
undermined by chronic staffing shortages and a contractor-oversight
framework with no meaningful monetary teeth. The Sailors reporting
unsanitary berthing, 19-hour repair shifts, and improvised sleeping on
mess-deck tables are not whining. They are telling the Navy — and the
taxpayer — what happens when immature technology is pushed to sea ahead
of its testing, and when habitability is treated as an afterthought.
The photograph released by U.S. 6th Fleet on 23 March 2026 showed a Super Hornet on Gerald R. Ford's
flight deck, stabilizers gleaming in Mediterranean sun. It was a
reassuring picture. It was also, in a narrow sense, a lie of omission.
Eleven days earlier, a fire in the carrier's aft main laundry space had
erupted in the ventilation and dryer-vent system. It burned for more
than thirty hours. Smoke migrated through the ship's overhead cableways
into seven adjacent berthing compartments. More than one hundred racks
were destroyed outright. Roughly six hundred Sailors were displaced from
their sleeping areas. Some slept on mess-deck tables. Some slept on the
deck. Over two hundred were assessed for smoke inhalation. And the
Navy's initial 12 March statement said only that the carrier "remained
fully operational" and that two Sailors had non-life-threatening
injuries.
Chief of Naval Operations Admiral Daryl Caudle later acknowledged, at the Center for Strategic and International Studies, that Ford
did not resume fixed-wing sorties for two days. The carrier eventually
limped to Naval Support Activity Souda Bay on Crete on 23 March, where
she remained pierside for more than a week of structural repairs, then
took a scheduled port visit in Split, Croatia, before re-entering the
Red Sea in late April in support of Operation Epic Fury against Iran. To
replace burned and smoke-contaminated bedding, the Navy stripped 1,000
mattresses from the pre-commissioning John F. Kennedy at
Newport News. Hull technicians procured roughly 2,000 sweatsuits and
other garments because most of the ship's laundry plant — the very plant
where the fire originated — was out of service, and the crew could not
wash what they were wearing. This is not an indictment of the
damage-control party. The Sailors did their job. It is an indictment of
what the Navy asked them to do it in.
A Pattern, Not a Coincidence
On 14 April, a fire aboard Dwight D. Eisenhower during her
Planned Incremental Availability at Norfolk Naval Shipyard injured — by
the Navy's own revised count — eight Sailors, not the three first
reported. On 19 April, a fire aboard Zumwalt at Ingalls
Shipbuilding in Pascagoula injured three more. Three ships. Three fires.
Fourteen injured Sailors. Six weeks. All three ships were either in a
maintenance availability or conducting extended operations under strain.
None of the causes has yet been publicly disclosed.
To understand why this pattern matters, one must read the Government Accountability Office's December 2025 report, Navy Ship Maintenance: Fire Prevention Improvements Hinge on Stronger Contractor Oversight
(GAO-26-107716). The report catalogs thirteen fires on Navy ships
undergoing maintenance since 2008, the worst being the July 2020 loss of
the amphibious assault ship Bonhomme Richard at Naval Base San
Diego — a $3-billion-plus write-off. GAO credits the Navy with real
post-2020 improvements in fire-safety culture. But it then delivers the
hammer: all three Navy organizations responsible for fire-safety
oversight during ship maintenance reported staffing shortfalls as of
March 2025. The Navy's primary contractor-compliance tool, the
Corrective Action Request, carries no monetary penalty. Quality
Assurance Surveillance Plans at the six ships GAO reviewed did not
assess penalties for contractor violations of safety standards. In plain
English: the bureaucratic mechanisms the Navy relies on to make
contractors take fire safety seriously do not impose costs on
contractors who do not. GAO made six recommendations. The Navy concurred
with all six. Eight weeks later, Eisenhower caught fire at Norfolk Naval Shipyard.
"Staffing shortages across key organizations mean more reliance on
sailors, who have other duties, to prevent fires. The Navy also uses
contract oversight tools to ensure ship maintenance contractors follow
safety standards. But these tools do not effectively enforce penalties
for safety violations."
— GAO-26-107716, 17 December 2025
The Ford's Plumbing Problem Is a Design Problem
Long before the laundry fire, Gerald R. Ford was already struggling to keep her crew in sanitary conditions. In July 2025, the mother of a Ford
Sailor provided photographs to Virginia public radio station WHRO
showing sewage overflowing onto berthing-compartment decks. Documents
obtained by National Public Radio under the Freedom of Information Act
tell the rest of the story. The carrier's Vacuum Collection, Holding and
Transfer system — a vacuum-based sewage plant adapted in part from the
cruise-ship industry to reduce freshwater use — has failed continuously
since the ship's first deployment in 2023. An undated Navy document
provided to NPR states bluntly that "every day that the entire crew is
present on the ship, a trouble call has been made for ship's force
personnel to repair or unclog a portion of the VCHT system, since June
2023."
The system divides roughly 650 toilets ("heads" in Navy parlance)
into ten independent zones. When a single valve fails at the back of a
single head, it can pull an entire zone's worth of heads offline for
half an hour to two hours. A March 2025 engineering-department e-mail
reviewed by NPR referenced 205 breakdowns in four days. Hull maintenance
technicians worked nineteen-hour shifts. Acid flushes to clear calcium
buildup in the undersized pipes cost roughly $400,000 apiece. The ship
called for off-ship technical assistance forty-two times between 2023
and early 2026; thirty-two of those calls came in 2025. The Government
Accountability Office flagged the VCHT design as undersized and poorly
specified in 2020. The Navy had no plans then to redesign it for the
follow-on John F. Kennedy (CVN-79). It still does not.
There is an institutional habit at work here. The 2020 GAO review
is a piece with the Director, Operational Test and Evaluation
(DOT&E) findings on Ford's flight-deck systems. The FY2024
DOT&E annual report — the most recent unclassified edition —
documents 8,725 EMALS shots and 9,266 arrested landings during Ford's
May 2023 to January 2024 deployment. It then states, in language
unusually pointed for an OSD test document, that "the reliability and
maintainability of CVN 78's EMALS and AAG continue to adversely affect
sortie generation and flight operations, which remains the greatest risk
to demonstrating operational effectiveness and suitability" in Initial
Operational Test and Evaluation. The crew, DOT&E noted, remains
reliant on off-ship technical support to correct EMALS, AAG, and
Advanced Weapons Elevator failures. Sortie-generation-rate testing — the
core measurement of what a carrier is for — has been deferred to FY2025 and now beyond. This after eight years in commission.
The Zumwalt: $25 Billion in Search of a Mission
If Ford is a cautionary tale about concurrency, Zumwalt
is a cautionary tale about the whole acquisition enterprise. The
Congressional Research Service and multiple GAO reviews put the
program's total life-cycle investment at roughly $25 billion for three
ships — a figure that works out to something in the vicinity of $8
billion per hull when research, development, and acquisition are rolled
together. The class was born as a twenty-first-century land-attack
destroyer built around twin 155-mm Advanced Gun Systems firing the Long
Range Land Attack Projectile. When the LRLAP's per-round cost exceeded
that of a Tomahawk cruise missile, the round was cancelled; the guns
became, functionally, ballast. In August 2023 Zumwalt entered
Ingalls Shipbuilding for a fundamental identity transplant: the forward
AGS mounts are being removed and replaced with four Advanced Payload
Module canisters capable of carrying up to twelve Conventional Prompt
Strike hypersonic missiles. She emerged from drydock in December 2024
and completed builder's sea trials in January 2026. Then, on the night
of 19 April 2026, she caught fire pierside.
The Navy has not disclosed the cause. What is known is that the
ship is at an especially sensitive moment in the integration of her CPS
components, that CPS live-fire testing from Zumwalt was
projected for 2027 or 2028, and that any meaningful damage to partially
installed, extraordinarily sensitive hypersonic-weapons integration
hardware could slip that date further. Three Sailors were injured. The
crew extinguished the fire without external assistance. That is a credit
to the damage-control organization. It does not answer the larger
question: what is a three-ship class — one of which has never
participated in combat operations — contributing to a fleet that the
Chief of Naval Operations has publicly acknowledged is running short of
ordnance after the Iran campaign, and short of carriers as Nimitz retires and Kennedy's delivery slips to March 2027?
What the Sailors Are Telling Us
The through-line across these stories is not any single technical
failure. It is that the burden of absorbing the consequences of those
failures falls — every time — on the most junior members of the crew. On
Ford, the average Sailor's age is similar to that of a college
sophomore. Many are on their first extended time away from home. They
are standing nineteen-hour watches fishing T-shirts and mop-heads out of
narrow VCHT pipework because the system was specified too small by a
shipbuilder to whom the Navy did not assign monetary penalties for the
deficiency. They are sleeping on mess-deck tables after a laundry fire
because habitability redundancy was not a design driver. They are
missing the birth of their first child during an
eight-month-stretched-to-eleven-month Caribbean and Middle East
deployment in which they cannot reliably use a toilet. Some have told
NPR they plan to separate after this cruise. The Navy's recruiting
environment cannot absorb that signal indefinitely.
The institutional response to these problems has, so far, been to
praise the resilience of the Sailors. Admiral Caudle's remarks at CSIS
were characteristic: "Sailors that are doing this, this is what they
signed up for." With respect to the CNO, they did not. They signed up to
fight the nation's wars at sea. They did not sign up to spend their
early twenties as a human buffer absorbing the cost of a twenty-year
acquisition failure.
Recommendations
Three actions are warranted, none of them novel:
First, the Navy must implement all six recommendations of
GAO-26-107716 on a published timeline, with milestones reported
quarterly to the House and Senate Armed Services Committees.
The Corrective Action Request process must be amended to include
monetary penalties for persistent contractor safety violations. Quality
Assurance Surveillance Plans must explicitly assess penalties for
noncompliance. The staffing shortfalls in the Regional Maintenance
Centers and Naval Surface Group fire-safety oversight billets must be
closed with dedicated billets, not by double-hatting Sailors whose
primary duties lie elsewhere.
Second, the Navy should commission an independent habitability review of Ford and Kennedy,
scoped to the VCHT system, berthing ventilation isolation, and
laundry-space fire suppression, with a plan of action and milestones for
retrofit.Kennedy is scheduled for delivery in March 2027. The same VCHT architecture that is failing on Ford is installed in Kennedy.
The 2020 GAO warning was ignored. The 2026 consequence is 600 Sailors
displaced and 1,000 mattresses pulled off the next carrier. There is
time, still, to fix this on CVN-79 before she sails. There will not be
time later.
Third, Initial Operational Test and Evaluation on Gerald R. Ford must be completed before additional Ford-class block-buy authorities are exercised.
Ten years into commissioning, DOT&E has still not been able to
evaluate sortie-generation rate or complete the Total Ship Survivability
Trial. The fleet is being asked to absorb a warship class whose core
performance claim has not been operationally validated. Concurrency was
the original sin of the Ford program. Doubling down on it in the FY2027
budget cycle would be the Navy's choice — not an inherited condition.
❦ ❦ ❦
Admiral Elmo Zumwalt — the officer for whom DDG-1000 is named —
devoted the latter part of his career to a simple proposition: that
enlisted Sailors deserve to live, work, and serve under conditions that
honor what the nation asks of them. He issued Z-grams. He integrated the
Navy. He dragged a fleet reluctantly toward treating its people as
people. The ship that bears his name is now a $4 billion testbed
awaiting its third reason for existence, with three Sailors recently
injured in a pierside fire of undetermined cause. The carrier that is
the Navy's flagship is returning to combat operations with sewage
problems its manufacturer refuses to redesign and fire-damaged berthing
still being repaired. This is not the fleet Admiral Zumwalt fought for.
It is a fleet that is asking its Sailors, once again, to pay in person
for choices made years earlier, in rooms they will never enter, by
people whose names they will never know. Proceedings owes them better.
So does the Navy.
Sources
All URLs verified as of 23 April 2026. Sources are listed in order of first reference.
The turboprop that won the counterterrorism era is not
the airframe that will win the next one — unless it is modernized around
the six mission threads the Pacific demands: assured PNT, laser C2,
boost-phase ISR, launched-effects teaming, long-range standoff strike,
and manned-unmanned coordination. All six are demonstrated. None are
integrated. The window to do it is now.
Palmdale · Yuma · Kadena · Vandenberg
Bottom Line Up Front
Tomorrow's war is not Afghanistan. It is a distributed,
electromagnetically contested, sensor-rich, missile-saturated Pacific
campaign fought across thousands of miles of water, with China fielding
4,000 hypersonic weapons by 2035 and Russian EW assets driving
thousand-flight-per-day GPS interference across NATO's eastern flank.
The MQ-9B has the endurance, payload, open architecture and production
base to matter in that fight — but only if it evolves along six
convergent axes already demonstrated in isolation: (1) assured PNT via
M-code EGI plus quantum magnetic navigation — with an MQ-9B composite
airframe whose paramagnetic aluminum-mesh LSP Faraday cage (selected by
GA-ASI for weight reasons against copper or nickel alternatives) sits on
the favorable side of the Tolles-Lawson permanent-magnetization problem
that dominates MagNav noise on metallic platforms like the F-16 and the
Cessna of the USAF/MIT MagNav Challenge, while shifting residual noise
into an eddy-current and EMI term that AI-augmented online calibration
is specifically engineered to handle; (2) optical C2 via GA-ASI's LAC-12
pod into SDA's Tranche 1 Transport Layer, where the first space-to-air
laser link to an aircraft-mounted terminal was closed on 1 July 2025;
(3) forward boost-phase ISR cueing HBTSS via improved Lynx radar and
MTS-B (which tracked ballistic missiles in a June 2016 USAF
demonstration); (4) launched-effects teaming through the PELE
semi-autonomous air vehicle (GA-ASI, June 2025) and future Increment 2
CCA variants; (5) long-range standoff strike with JASSM, LRASM and JSM
integration now underway (GA-ASI, February 2026); and (6)
human-on-the-loop teaming with F-22/MQ-20, F-35/CCA, and
P-8/SeaGuardian, all demonstrated in the last eighteen months. The MQ-9
production line is hot through 2026. The decision before the Air Force,
Navy and Marine Corps is whether the aircraft is a legacy platform
winding down, or a distributed-operations node being actively evolved.
This is the case for the latter.
The War We Are Actually Preparing For
The temptation after Operation Epic Fury is to declare
the medium-altitude long-endurance turboprop obsolete. The data is
seductive: roughly 24 MQ-9 airframes lost to Iranian air defenses in six
weeks, at a replacement cost of about $720 million — 8% of the Air
Force's 300-aircraft Reaper fleet attrited while flying a mission the
airframe was never designed for. The International Institute for
Strategic Studies noted last November that the Houthis' patchwork SAM
network alone has chewed through at least 15 MQ-9s since late 2023.
Against S-400, Bavar-373, or anything China would field in a Taiwan
Strait scenario, the Reaper's 230-mph cruise and non-stealthy profile
are exactly as survivable as critics say they are.
But the war for which the MQ-9B needs to evolve is not the
penetration fight. The Air Force is building the YFQ-42A Dark Merlin and
YFQ-44A Fury for that. The B-21 is being built for that. Tomorrow's
fight, for the airframe already in inventory, is the distributed Pacific
problem — persistent maritime ISR, anti-submarine warfare,
electromagnetic sensing, targeting cueing for long-range fires, and data
transport across an Agile Combat Employment archipelago where crewed
assets cannot loiter indefinitely and where the tyranny of distance
makes endurance the scarcest commodity in the theater. The MQ-9B has, in
its MQ-9B SeaGuardian/SkyGuardian configuration, 30-to-40 hours of
endurance depending on payload, a 50,000-ft ceiling, and proven
performance above the 78th parallel — where satellite coverage is
thinnest and where the Arctic is becoming a major theater of PLA
submarine activity.
In February 2026, Asia Times and the South China Morning Post
reported that the U.S. was expanding a network of MQ-9s across the
Indo-Pacific, knitting Japan (doubling Coast Guard MQ-9Bs to 10,
ordering 23 SeaGuardians by 2032), Taiwan (four on order, two delivered
March 2026), Australia, Belgium, India (31 more ordered), and others
into a shared ISR architecture that CSBA has called "deterrence by
detection." That concept is not premised on airframe survivability in a
shooting war. It is premised on persistent, multinational, attributable
surveillance creating escalation costs in peacetime and fire-control
quality targeting data in wartime. The MQ-9B is the platform of record
for that mission. The question is not whether to retire it. The question
is how to evolve it.
The MQ-9B's future is not as a hunter-killer or as a penetrator. It is
as a persistent, distributed, laser-linked, launched-effects-carrying node
in an allied sensor-and-shooter architecture stretching from the Arctic
to the South China Sea. Every element needed is demonstrated. None are
integrated. Integration is the program.
Six Axes of Evolution
I. Assured PNT
Russian jamming forced a USAFE Reaper to make an emergency landing
near Mirosławiec, Poland, in March 2024. U.S. officials attributed a
portion of the Epic Fury losses to Iranian high-power GPS spoofing and
jamming of satellite command links. The MQ-9's current Honeywell H-764
EGI was SAASM-qualified before M-code receivers were available for the
fleet, and its command-link architecture was built around a single
commercial Ku-band geostationary pipe. Neither holds up under peer or
near-peer electronic attack.
The fixes exist. On 20 November 2025, Honeywell received MSO-c145b
authorization from the Precise Position Equipment Certification Office
for its small-form-factor FALCN-M M-code embedded GPS/INS, completing
the M-code qualification for Honeywell's full EGI line. The MQ-9 M2DO
(Multi-Domain Operations) configuration, first flown in November 2022
and under retrofit through FY26 via the System Lifecycle Agile
Modernization (SLAM) program, specifies anti-jam GPS, Link 16, IP-based
mission architecture and enhanced C2 resiliency. Backing this up,
Q-CTRL's Ironstone Opal quantum magnetic-anomaly navigation system,
flown in February 2025 near Griffith, Australia, delivered positioning
accuracy up to 111× better than a strategic-grade INS in GPS-denied
conditions — using only publicly-available magnetic anomaly maps and
fusing a quantum scalar magnetometer with a classical vector fluxgate
and an INS through an AI-driven denoising algorithm. DARPA's Robust
Quantum Sensors (RoQS) program is funding the ruggedization. Lockheed
Martin and Q-CTRL hold a March 2025 DoD Defense Innovation Unit contract
for a quantum-enabled inertial navigation prototype.
The MQ-9B airframe presents a more nuanced advantage for MagNav than
first appears, and it is worth getting the physics right. The airframe
is built to NATO STANAG 4671 standards primarily from advanced
graphite-epoxy and related composite materials, with metallic primary
structure confined to hardpoints, engine mount, landing gear and the
immediate vicinity of high-load joints. Compared to the predominantly
aluminum airframes on which virtually all published MagNav research has
been conducted — the Cessna Grand Caravan of the USAF/MIT Signal
Enhancement for Magnetic Navigation Challenge, the F-16 of the AFIT
online-calibration thesis work, and the Cessna Citation 560 used for the
Northrop EGI-M validation flights — the carbon-epoxy structure presents
a significantly lower ferromagnetic noise floor. There is less
steel, less iron in the primary structure, so less permanent
magnetization and a weaker induced-magnetization response to the Earth
field as the aircraft maneuvers. Q-CTRL's own public characterization of
the metallic-platform problem is blunt: "the fact that the airplane is
made of metal, with all this wiring… usually there's 100 to 1,000 times
more noise than signal."
The catch, which anyone who has walked the Poway manufacturing floor
will recognize from the smell of epoxy curing, is that STANAG 4671
certification requires lightning strike protection — and GA-ASI's
implementation, consistent with the weight-driven choice Cirrus made for
the SR-20/22 and the broader MALE industry practice, is an expanded
aluminum mesh embedded in the outer laminate ply and electrically bonded
to internal metallic ground planes to form a continuous Faraday cage
distributed across the full skin. The weight penalty for aluminum is
roughly half that of copper per unit area of equivalent
lightning-current capability, which on a fuel-fraction-driven
long-endurance airframe is not a negotiable tradeoff.
Aluminum's magnetic properties are almost ideal for a MagNav
platform. Its relative permeability is μᵣ ≈ 1.000022 — paramagnetic to
within 22 parts per million of vacuum — which is to say it contributes
essentially zero to the Tolles-Lawson permanent-magnetization and
induced-magnetization terms that dominate noise on a carbon-steel or
nickel-bearing structure. Compare that to 316L austenitic stainless at
μᵣ ≈ 1.003-1.007, or to nickel-plated carbon fiber LSP alternatives
where μᵣ is in the hundreds. On those permanent and induced terms, the
MQ-9B sits on the cleanest end of the spectrum available to any
certificated aircraft configuration.
The aluminum mesh does carry eddy currents. Every aircraft attitude
change induces currents in the continuous skin, and those currents
generate their own time-varying magnetic fields — the third
Tolles-Lawson term, which the calibration model exists to compensate.
Aluminum's electrical conductivity at roughly 60% IACS (against copper's
100%) means those currents are proportionally weaker than they would be
in a copper mesh of equivalent geometry. The LSP system is also tied to
the internal avionics ground plane, which means motor commutation,
power-converter switching, and digital clock harmonics have a
low-impedance conductive path onto a distributed skin antenna that sits
physically close to any magnetometer not mounted on a tail stinger — and
a MALE mission profile will not tolerate carrying a stinger.
The net effect shifts which noise component dominates, rather than
eliminating noise entirely. On an aluminum F-16 or a Cessna Caravan,
permanent and induced ferromagnetic magnetization dominate and produce
Q-CTRL's cited 100-to-1,000× noise-over-signal ratio. On a composite
MQ-9B with paramagnetic aluminum LSP mesh, eddy-current and skin-return
EMI terms dominate, but the ferromagnetic floor is fundamentally lower.
That shift is favorable for two reasons. First, the eddy-current
response of a fixed, known-geometry aluminum mesh is linear in aircraft
rate, spatially structured, and repeatable flight-to-flight in a way
that randomly-distributed ferromagnetic inclusions are not. Second, the
machine-learning online-calibration architectures that have matured
between 2023 and 2026 — the Physical Review Applied reservoir-computing
work, the arXiv Liquid Time-Constant Network approach published January
2024, and the March 2026 neural-network-augmented EKF with cold-start
capability — are designed specifically to handle platform-specific EMI
and eddy-current signatures that conventional Tolles-Lawson cannot
characterize. Q-CTRL's Ironstone Opal architecture is one instantiation
of this; it explicitly pairs a quantum scalar magnetometer with
AI-driven denoising to strip out platform noise. An MQ-9B makes this
tractable because the LSP mesh geometry is fixed and known by design,
the mesh is paramagnetic aluminum, and the 30-hour endurance gives the
online-calibration filter the operational dwell time it needs to
converge.
An MQ-9B with M-code EGI, quantum MagNav calibrated for its specific
aluminum-LSP signature, and a terrain-referenced-navigation vision
backup has four independent position references. Today's Reaper has one.
And the airframe on which the MagNav solution runs lands on the
physics-favorable side of the permanent-magnetization problem — the hard
one — in a way no metallic fixed-wing platform on which the technique
has been flight-tested to date can match.
Why Aluminum LSP Mesh Is the Right MagNav Compromise
The MQ-9B's STANAG 4671 certification for European civil airspace
required an engineered lightning strike protection system. GA-ASI's
weight-driven choice of expanded aluminum mesh — embedded in the
outermost laminate ply under the surface film, in electrical contact
with internal metallic ground planes (engine, conduit, avionics chassis,
fasteners) to form a continuous low-impedance path for 200,000-amp
lightning current — is the same choice Cirrus made on the SR-20/22 and
that much of the CFRP aircraft industry has converged on. Copper mesh is
denser and introduces galvanic corrosion issues against carbon fiber
that require an isolation ply adding still more weight. Aluminum was
chosen for weight. That decision happened to optimize for MagNav as
well.
The physics consequences separate cleanly. Aluminum is paramagnetic
at μᵣ ≈ 1.000022 — twenty-two parts per million of vacuum — meaning it
contributes essentially zero to the permanent and induced magnetization
terms that dominate MagNav noise on metallic aircraft. The MQ-9B's total
ferromagnetic signature is carried almost entirely by the engine,
landing gear, wiring harnesses, and hardpoint metal, with the LSP skin
contributing nothing to the static-field problem. The ferromagnetic
noise floor is fundamentally lower than on any aluminum-airframe
aircraft on which MagNav has been flight-tested. The eddy-current term
is real but bounded: aluminum's 60% IACS conductivity produces
proportionally weaker induced currents than copper mesh of equivalent
geometry would, and the mesh is a fixed, known-by-design conductive
sheet rather than randomly-distributed ferromagnetic inclusions.
Three things make the residual eddy-current and EMI coupling
tractable. First, the LSP geometry is structured and repeatable —
precisely what modern online-calibration filters are built for. Second,
AI-augmented calibration stacks (the Liquid Time-Constant network
published January 2024, the neural-network-augmented EKF with cold-start
capability published March 2026, Q-CTRL's Ironstone Opal) have
demonstrated 58-64% compensation error reductions over classical
Tolles-Lawson on metallic-airframe MagNav Challenge datasets; those
gains should be larger on a paramagnetic-skin platform. Third, the
MQ-9B's 30-hour endurance gives the filter the convergence time it needs
under operational profiles. The aluminum mesh is a compensation
problem. It is not a deal-breaker. Combined with the composite primary
structure, it makes the MQ-9B the best candidate in the Western
inventory to be the reference platform for operational airborne MagNav.
II. Optical C2 and the Tranche 1 Handshake
The single most important development for the MQ-9B's future does not
involve the airframe at all. On 1 July 2025, the Space Development
Agency closed the first-ever space-to-air optical communications link —
between a General Atomics Electromagnetic Systems OCT mounted on an
aircraft and a Kepler Communications satellite at roughly 500 km LEO.
SDA's Nathan Getz, director of the agency's Data Transport Cell, told
reporters in September that the link was ready to be folded into
operational tranches. By that point, Tranche 1 was already flying: 21
York-built Transport Layer satellites launched 10 September 2025,
another 21 Lockheed-built on 15 October 2025, on the way to a full
constellation of 126 Transport and 35 Tracking satellites across ten
Falcon 9 missions. On 20 January 2026, SDA declared the laser mesh
operationally — a proliferated LEO backbone treating optical
inter-satellite links as the primary data-transport layer, not RF.
GA-ASI's optical pedigree maps directly onto that architecture. The
company's Airborne Laser Communication System (ALCoS), developed under
internal funding over five years, closed an air-to-space link from
Tenerife to TESAT's LCT 135 terminal on the Alphasat GEO satellite in
February 2020 — the first demonstration of an air-to-space lasercom
system with SWaP compatible with a MALE RPA. In June 2021, SDA
contracted GA-EMS to integrate its LINCS laser terminal pair with an
MQ-9 for a space-to-air experiment. On 26 September 2022, GA-ASI flew a
1.0 Gbps air-to-air optical link near Yuma, exchanging real-time
navigation, video, and voice data. On 1 December 2022, the company
demonstrated a fully-networked multi-terminal lasercom mesh. The LAC-12
Laser Airborne Communication Terminal is now a marketed, podded,
open-architecture product offering 300× the data capacity of RF SATCOM,
explicitly sold as integrable on MQ-1 and MQ-9.
A LAC-12-equipped MQ-9B plugged into Tranche 1's SIS-002-compatible
optical mesh is a different animal from a Ku-band Reaper. It is a
sub-second-latency, multi-Gbps, LPI/LPD-linked node in the same network
that L3Harris's HBTSS demonstrator uses to deliver fire-control-quality
data to Aegis and the future Glide Phase Interceptor. It is also immune
to the Iranian jamming that produced a "total link failure" scenario
reportedly responsible for at least some Epic Fury losses.
III. Forward Boost-Phase ISR
The Defense Intelligence Agency's May 2025 "Golden Dome for America"
assessment warned that China may already have deployed a hypersonic
glide vehicle capable of striking Alaska, and projected a stockpile of
4,000 hypersonic weapons by 2035. MDA Director Lt. Gen. Heath Collins
has publicly acknowledged that the Glide Phase Interceptor program is
running roughly three years behind schedule, with delivery pushed toward
2035 under current funding. Near-term Guam and Pacific defense leans on
SM-6 and THAAD terminal engagement, augmented by HBTSS tracking from
LEO. The gap in this layered architecture is the airborne sensor layer —
persistent, forward-deployed surveillance close enough to probable
launch regions to catch transporter-erector-launcher (TEL) movement and
confirm space-based detections.
The MQ-9B fills exactly that gap, using sensors already in the
airframe. The Lynx multi-mode radar — in its AN/APY-8A Block 20A and
AN/DPY-1 Block 30 configurations, derived from Sandia's original
architecture — operates in Ku-band with spotlight SAR resolution to four
inches, stripmap mosaic modes, Coherent Change Detection (CCD) for
pixel-level scene differencing between passes, Amplitude Change
Detection, Automated Man-Made Object Detection, Ground and Dismount
Moving Target Indicator capable of flagging 1-mph personnel movement,
and the DARPA Dual-Beam Space Time Adaptive Processing upgrade developed
with BAE Systems that cancels main-beam GMTI clutter to detect slow
movers at tactically significant ranges. GMTI scans 270 degrees. MWAS
correlates AIS with radar returns for maritime targets.
Paired with the MTS-B Multispectral Targeting System — EO/IR,
shortwave infrared, image-intensified TV, laser designator/illuminator,
fused video — the Lynx/MTS-B combination provides oblique optical and
radar angles from the edge of adversary airspace that HBTSS cannot
achieve from LEO. Two MQ-9s demonstrated ballistic-missile tracking
using the MTS-B turret during a USAF exercise in late June 2016 — a
capability MDA has expressed interest in exploiting since 2011 for
firing-quality data on early intercept of ballistic launches. What was
missing was the low-latency link to a fire-control system. Tranche 1
provides it. An improved Lynx with tightened CCD processing,
wider-bandwidth Dual-Beam STAP, and tighter cross-cue timing to MTS-B
SWIR — running CCD on 3-hour intervals over known TEL hide sites,
slewing MTS-B to SWIR plume detection the moment ignition occurs,
compressing and pushing the track through LAC-12 into the optical mesh —
is a boost-phase sensor node in everything but name.
IV. Launched-Effects Teaming
The survivability objection — that a Reaper at 200 nm standoff still
can't see close enough to matter — is answered by launched effects. In
June 2025, GA-ASI unveiled PELE (Precision Exportable Launched Effect),
an 11-ft-wingspan, 16-hp, propeller-driven, semi-autonomous air vehicle
with an EO/IR full-motion video sensor and internal modular payloads,
range exceeding 500 nm, designed specifically to be launched from MQ-9B
SkyGuardian/SeaGuardian. GA-ASI President David Alexander's articulated
concept of operations is explicit: "An air force could launch MQ-9Bs for
long-endurance ISR patrols one day and deploy the same aircraft the
next day with several PELEs that take on the highest-risk roles,
preserving the mothership." A SkyGuardian approaches a contested ADIZ
from international waters, releases multiple PELEs, and those vehicles
penetrate the threat envelope to detect and geo-locate radar emitters,
confirm adversary composition, or deliver effects — while the host
aircraft remains outside the SAM ring.
This is the architectural escape from the Epic Fury attrition curve.
The MQ-9B becomes a persistent launch base and data-fusion hub for
attritable, distributed sub-elements that do the risky work. The same
principle applies to the X-68A (Dark Merlin/LongShot) uncrewed
air-superiority vehicle designated by the Air Force in February 2026.
CCA Increment 2 and beyond will push this further — the MQ-9B is one
generation of airframe that can act as a standoff mothership for the
next generation of autonomous combatants.
V. Long-Range Standoff Strike
On 23 February 2026, GA-ASI announced that engineering work was
underway to integrate AGM-158 JASSM, AGM-158C LRASM, and
Kongsberg/Raytheon JSM on the MQ-9B airframe. The notional concept of
operations, articulated in the company's own words, is the Western
Pacific standoff case: "MQ-9Bs could launch from a number of friendly
bases in the Western or Southern Pacific, fly to a hold point and loiter
there outside a hostile power's weapons engagement zone. If the order
came to release the weapons, the aircraft could launch them in
coordination with other U.S. or allied operations." First-round
captive-carry flight tests are targeted for 2026. This changes the
arithmetic. A persistent MALE airframe loitering 500 nm from a Chinese
coast, launching JASSM-ER (~600 nm range) or LRASM against surface
action groups on organic or cross-cued targeting, is not the Reaper of
Afghanistan. It is a distributed missile truck with a 30-hour
persistence that crewed strike platforms cannot match.
Paired with the improved Lynx MWAS mode and SeaGuardian's AIS
correlation, the MQ-9B becomes the sensor-shooter pair for anti-surface
warfare in the littoral Pacific. Ultra Maritime's compact sonobuoys and
receivers, successfully flight-tested on SeaGuardian in January 2025,
extend the same architecture to anti-submarine warfare — including in
GPS-denied environments where GA-ASI's own press release specifies the
sonobuoy receivers must function. Airborne early warning capability is
slated for demonstration on MQ-9B in summer 2026.
VI. Manned-Unmanned Teaming
The sixth axis is the one that integrates all the others. In 2025,
GA-ASI flew an internally-funded Avenger demonstration that featured
both its own TacACE autonomy software and Shield AI's Hivemind software
on the same flight, with the MQ-20 switching between AI pilots in
mid-air. Later in the year, a separate demonstration with Lockheed
Martin and L3Harris connected an MQ-20 with an F-22 Raptor — allowing
the human fighter pilot to command the unmanned aircraft as a CCA
surrogate via tablet from the cockpit. In January 2026 GA-ASI flew an
MQ-20 mission autonomy demonstration in which the aircraft independently
ranged, tracked, and simulated a weapons engagement against a live
piloted aggressor. In March 2026, GA-ASI and the Air Force conducted an
autonomous mission at Edwards using infrared-based passive target
localization and autonomous coordination between manned fighters and
unmanned jets. The Navy's Naval Air Warfare Center Aircraft Division
completed an F-35/CCA teaming demonstration in January 2026 at Point
Mugu using F-35 pilots controlling autonomous BQM-177As via touchscreen
tablet.
At Sea-Air-Space 2026, GA-ASI outlined P-8 Poseidon/SeaGuardian
teaming as a specific operational pairing — crewed maritime patrol
aircraft for persistence-limited high-intensity ASW work, SeaGuardian
for long-dwell sonobuoy deployment and monitoring. The architecture is
generalizable: F-22 or F-35 commands a Reaper-class platform at
standoff; the Reaper commands a PELE swarm or a CCA Increment 2
formation; the CCA swarm penetrates. The Reaper is the middle layer.
That is the layer the service most needs and currently least has.
The Evolved MQ-9B Architecture
Navigation
Honeywell
FALCN-M M-code EGI (MSO-c145b certified Nov 2025); Q-CTRL Ironstone
Opal quantum magnetic-anomaly navigation (DARPA RoQS) with AI-augmented
online calibration characterized for the MQ-9B's specific STANAG 4671
paramagnetic aluminum-mesh LSP signature; vision-based
terrain-referenced navigation backup; seabird-inspired multi-cue fusion
arbiter running on mission computer.
C2 & Data
GA-ASI
LAC-12 Laser Airborne Communication pod into SDA Tranche 1 Transport
Layer optical mesh; Starlink/Starshield LEO SATCOM backup; Ka-band
O3b/Inmarsat; HF BLOS via FlexRadio FLEX-6600 SDR through conformal tail
antennas (8,000 nm); legacy Ku-band GEO as fallback.
Sensors
Improved
Lynx Block 30+ (CCD, ACD, AMMOD, DMTI/GMTI, MWAS, Dual-Beam STAP);
MTS-B EO/IR/SWIR/laser designator with boost-phase cross-cue; sonobuoy
dispensing system for ASW; electronic support measures pod for ELINT.
Weapons
AGM-158
JASSM-ER, AGM-158C LRASM, Kongsberg/Raytheon JSM (integration underway,
2026 captive-carry); Hellfire and laser-guided bombs for legacy
missions; AIM-9X for self-defense if integration continues.
Launched Effects
PELE
semi-autonomous air vehicles (11-ft wingspan, >500 nm range, EO/IR
FMV), multiple per sortie for ADIZ penetration and ELINT; Altius 600
loitering munitions; future X-68A LongShot integration.
Autonomy
GA-ASI
Quadratix ground environment; TacACE and Hivemind-class autonomy for
lost-link mission continuation, multi-aircraft control by single
operator, and manned-unmanned teaming under F-22/F-35/P-8 command via
tablet.
What the Composite Airframe Costs and What It Buys
The structural properties that make the MQ-9B's composite airframe
favorable for laser-link pointing, MagNav signature management, and
sensor-to-antenna registration also impose the same manufacturing and
sustainment discipline that has defined composite airliner production
since the 787 entered service. Unlike aluminum, which accommodates
assembly error through elastic compliance — a quarter-inch misalignment
gets pulled into place with rivet tension, and the skin deforms to match
the frame — cured graphite-epoxy will not permanently deform to absorb
fit-up mismatch. Aviation Week put it directly in its 2022 coverage of
the 787 program: "composite structures are very stiff, unlike
conventional aluminum airframes, which are flexible. Any issues that
potentially interfere with the load transfer between sections — such as
gaps, improperly installed shims or inner skin surfaces that are not
smooth — can form a focus for stress buildup." Boeing's own published
join-surface flatness tolerance on the 787 is 0.005 inch — "about the
thickness of a human hair."
The industry's solution is a two-part manufacturing discipline that
the MQ-9B program inherits. Precision surface preparation: on the F-35,
every composite joining surface is CNC-machined after autoclave cure to
guarantee outer-mold-line tolerance. Predictive shimming: on the 787,
robotically-placed laser scanners map each mating surface, software
generates required shim geometry, and resin-bonded composite shims fill
gaps per Boeing Process Specification BAC5430. The 47/48 aft fuselage
join alone carries over 2,000 fasteners and required through-hole
inspection with angled feeler gauges when predictive shimming failed in
2019-2022. A March 2026 FAA proposed Airworthiness Directive mandates
recurring inspection of 787 splice plates, spar terminal fittings and
chords for fatigue cracks traceable to out-of-tolerance shim gaps. These
are not niche issues — they are the central ongoing quality story in
composite airliner production, and they apply, in smaller scale but
identical physics, to every MQ-9B coming off the Poway and El Mirage
lines.
For the MQ-9B's evolution, this cuts four ways. The first is
structural: once cured and assembled, the composite airframe is
dimensionally stable under flight loads in a way aluminum is not.
Aluminum wings flex continuously in flight, which is why they fatigue on
a cycle-count basis and why skin-mounted sensors on aluminum platforms
require active pointing compensation for structural breathing. A LAC-12
optical terminal trying to close an air-to-space laser link with
microradian pointing tolerance, or an improved-Lynx antenna cross-cueing
MTS-B to SWIR plume detection, or a magnetometer sensing at the
nanoTesla level — none of those want to be mounted to a structure that
oil-cans and torsions under every turbulence encounter. Boeing's own 787
full-scale fatigue test logged "zero findings in fatigue in our
composite structure" over 165,000 simulated flights, even on an article
that — as was later discovered — contained the same production
nonconformances that affected the first 980 delivered aircraft. That is a
remarkable robustness statement about cured composite primary structure
when the as-built geometry is held. The composite airframe's stiffness
is what makes the laser-link and boost-phase ISR axes of this evolution
architecturally plausible in the first place.
The second is battle-damage repair. A combat-damaged aluminum
Reaper could in principle be field-patched at a forward operating
location with hand tools and a rivet gun. A combat-damaged MQ-9B with
skin damage is a depot-level repair — the damaged area must be ground
out, a pre-cured scarf patch fabricated to the exact local geometry and
fiber orientation, and the assembly vacuum-bag hot-bonded (or
autoclave-cured) under controlled conditions. Field kits for minor
composite damage exist; structural battle-damage repair does not
transition to expeditionary bases cleanly. This is a real constraint on
the Agile Combat Employment dispersal concept and one that argues for
theater-level composite depot capacity at Kadena, Andersen, or an allied
MRO partner.
The third is retrofit modification. Cutting new access panels,
adding hardpoints for new payloads, integrating a different antenna
array — every one of these requires local laminate characterization,
engineered stress analysis for the cutout, and often a cure cycle to
embed doublers. The six-axis evolution this article argues for is not
rivet-and-fly work; it means coordinated engineering changes at El
Mirage and Poway flowed into a block-upgrade configuration with
engineered retrofit kits executed at depot. GA-ASI's completion of
full-scale MQ-9B fatigue testing in November 2025 provides the
structural certification baseline — the MQ-9B equivalent of the 787's
165,000-cycle validation — that makes those modifications qualifiable
against validated as-built properties. The January 2026 El Mirage
expansion for MQ-9B production and testing points to the same
industrial-scale infrastructure build-out that Boeing Charleston and
Spirit Wichita required for the 787 program. A block upgrade rather than
an evolutionary in-service modification path is the correct
programmatic model.
The fourth is allied interoperability. The growing multinational
MQ-9B fleet — Japan (10 MQ-9Bs plus 23 SeaGuardians by 2032), Taiwan
(four on order, two delivered March 2026), India (31 more ordered),
Australia, Belgium, and others — cannot all retrofit through Poway. The
programmatic answer is qualified allied composite depots: established
MRO partners in Australia and the UK, and the 20 January 2026
GA-ASI/Calidus MOU for co-production of MQ-9B and Gambit in the UAE. Any
block-upgrade kit design must be manufacturable and installable at
multiple authorized facilities, not just at Poway, and each facility
must be qualified to the same BAC5430-equivalent shimming and
surface-preparation discipline that Boeing imposes on 787 suppliers.
The headline tradeoff: composite construction imposes tight
manufacturing and sustainment tolerances as the price of operational
precision. The 787's shim-gap saga is the industry's long education in
what that costs when quality discipline slips. For an aircraft whose
future mission is persistent sub-microradian laser pointing to LEO,
nanoTesla-level MagNav sensing, and millimeter-level antenna-to-turret
sensor registration, the stiffness that makes retrofit difficult is the
same stiffness that makes the evolution mission architecturally
possible. But the programmatic model has to acknowledge it: the six-axis
MQ-9B is not an aluminum-airframe modernization effort. It is a
block-upgrade configuration baseline with depot-level retrofit flowed
through a qualified multinational supply base, executed under the same
composite manufacturing discipline the 787 program learned at
significant cost. Nothing about that is impossible. Everything about it
requires treating the airframe's manufacturing properties as a
first-order constraint on the program plan.
The Third-Party Structural Spares Problem
There is a second-order programmatic consequence of the composite
airframe that has not received the attention it deserves in the MQ-9B
sustainment discussion, and it is cleaner to state directly: the
traditional third-party Parts Manufacturer Approval (PMA) ecosystem —
the distributed aftermarket that has supplied the Western fleet with
aluminum structural spares since the DC-3 era — is not entering
composite primary structure. Conversations with established PMA houses
active in aluminum structural work reveal that these companies are
explicitly choosing not to pursue PMAs for composite structural
components on the new generation of airframes. That choice has concrete
economic drivers that the services need to confront.
The aluminum-era PMA business model rests on pillars that do not
transfer to composite primary structure. An aluminum skin panel can be
reverse-engineered from dimensional inspection of the OEM part, tested
for tensile and fatigue properties in standard coupon work, and
demonstrated to FAA satisfaction through identicality or comparative
analysis in months under 14 CFR Part 21 Subpart K. A composite
structural part cannot be reverse-engineered from the finished article
alone — the ply sequence, ply orientation, fiber/resin chemistry, cure
cycle, void content, and as-cured dimensional tolerances are not
externally observable, and each is an independent engineering variable
that affects certified strength. A PMA applicant would need the OEM's
proprietary design allowables database, layup drawings, and process
specifications to match the OEM part, and OEMs do not share those. FAA
Order 8110.48A, "Composite Aircraft Parts Approvals," codifies the
substantiation framework but does not reduce its cost.
The cost itself is the second barrier. CompositesWorld noted in
2015 that "the certification of aerospace composite products for human
flight is still driven by exhaustive experimental testing" and that
major aircraft OEMs "spend millions of dollars and allocate thousands of
man-hours annually to test and retest designs for certification." A PMA
shop operating on a few percent of OEM list price cannot amortize a
building-block test campaign — coupon, element, subcomponent, full-scale
component — across an expected aftermarket volume that is, for a
300-airframe military fleet, inherently small. The third pillar is
capital intensity: composite primary-structure fabrication requires
autoclaves, automated fiber placement equipment, controlled-environment
clean rooms, engineered matched tooling, and at minimum ultrasonic
C-scan non-destructive inspection capability that legacy PMA houses do
not operate and cannot justify building without an OEM license or a
large captive repair market. The fourth is liability: a
reverse-engineered aluminum bracket that fails produces contained
damage; a reverse-engineered composite wing skin that delaminates in
service under load is a potential hull-loss event, and the insurance and
legal exposure reflects that.
The industry response has been concentration rather than
distribution. Composite primary-structure work gets done by a small
number of vertically-integrated specialty houses — Comtek (a Latécoère
subsidiary, operating as both Approved Maintenance Organization and
Design Approval Organization), HAECO Composite Services, Evans
Composites, DAS Aviation with its dual onsite autoclaves, and a handful
of others — generally as repair organizations with in-house DERs, rather
than through the diffuse PMA ecosystem that sustained aluminum-era
fleets. The Commercial Aircraft Composite Repair Committee, founded in
1991 by consolidating A4A, IATA, and SAE repair task forces,
standardized composite repair practice but explicitly did not create a
replacement-parts manufacturing pathway. These are repair shops. They
are not structural-spares suppliers. The market segment that would sell
you a third-party MQ-9B wing skin essentially does not exist in the
composite era, and — as your industry contacts are confirming — the
companies that could in principle enter it are deliberately staying out.
The military sustainment consequences are significant. Since Desert
Storm, the Air Force has relied on a healthy aftermarket PMA ecosystem
to handle surge demand during combat attrition. When MQ-9A losses over
Iraq and Afghanistan drove up replacement demand, third-party PMA shops
absorbed a meaningful fraction of the aluminum-structure spares load.
When Epic Fury attrition is backfilled with composite MQ-9Bs, that surge
capacity vanishes unless GA-ASI Poway/El Mirage, or a licensed allied
co-producer under an arrangement like the January 2026 GA-ASI/Calidus
MOU, builds it. A sustained high-tempo campaign with significant
composite-airframe attrition would bottleneck on OEM production capacity
in a way that aluminum-era operations did not. This is a fundamentally
different sustainment posture from anything the services have operated
under before.
The historical analogy worth drawing is the B-52 sustainment model,
which has kept Boeing's 1950s-era heavy bomber flyable for seven
decades and is projected to carry it through 2050 under the current
Commercial Engine Replacement Program. Kelly Air Force Base — now Port
San Antonio — has been the B-52 sustainment hub for most of that period,
and the work includes cases where Boeing's original engineering
drawings for specific components were lost or never fully preserved
(Boeing's own B-52 program materials acknowledge that the aircraft was
"designed with pencils and paper in the 1950s"). For aluminum structural
spares in that situation, the solution was straightforward: engineering
services contractors based at or near Kelly — including CACI's San
Antonio operation — reverse-engineered replacement parts from surviving
articles using dimensional inspection, metallurgical analysis, and
coupon testing, substantiated them under PMA or equivalent government
procurement pathways, and kept the fleet in the air. That business
existed because the underlying aluminum parts could be
reverse-engineered at all. Composite primary structure on an MQ-9B
retained through 2050 would offer no comparable pathway if GA-ASI's
original engineering data for a given production lot is ever lost —
through corporate restructuring, archive obsolescence, proprietary
format decay, or any of the mundane ways engineering records disappear
over decades. You cannot rebuild a composite wing skin from dimensional
inspection of the surviving article. The ply sequence, orientation,
fiber/resin chemistry, and cure history are internal to the part and
invisible to external measurement. The B-52's aluminum structure has
been the single cleanest case study in long-horizon Western military
aircraft sustainment precisely because aluminum forgives the loss of the
engineering data package in a way composite primary structure does not.
A closer recent precedent is the F-117 program, which operated under
exactly this constraint for a different reason — specialty coatings and
stealth geometry requirements meant only Lockheed Skunk Works could
produce structural replacements, and wartime attrition was expensive in
consequence. The 787 and A350 created that same concentrated-supply
dynamic across the widebody commercial fleet. The MQ-9B brings it into
the MALE unmanned sustainment model. Fleet planners across the allied
MQ-9B operators — the US Air Force, US Marines, UK RAF, Japan (with its
planned 33-aircraft fleet), Australia, Belgium, Taiwan, India — will
have to confront that the composite-airframe choice that enables the
six-axis evolution also binds them to a narrower, OEM-concentrated
supply base than any Western tactical aircraft program that relied on a
healthy third-party aftermarket. No amount of FAA rule-making will
conjure a PMA market the economics do not support. The policy answer, if
there is one, lies in deliberately standing up licensed allied
composite-structure production through arrangements like Calidus, funded
OEM capacity expansion through DPA Title III investments, mandated
long-term archival of as-built engineering data packages against future
sustainment needs, and forward-deployed theater depot composite
capability with enough captive autoclave and AFP equipment to handle
surge loads in the Indo-Pacific. None of this is in any published MQ-9B
program plan the open literature has made visible. The composite-spares
constraint is real, it is going to bite, and the time to address it is
before the next Epic Fury rather than after.
Programmatics: A Block Upgrade, Not a Hope
Most of this is already funded somewhere in the defense enterprise.
M-code EGI is certified and available. Quantum MagNav is under DARPA and
DIU contract. LAC-12 is a marketed product; the Tranche 1 mesh is on
orbit. JASSM/LRASM/JSM integration is GA-ASI-funded and underway. PELE
is flying. Autonomy software is mature across TacACE, Hivemind, and
Collins Aerospace's Sidekick (which flew the YFQ-42A's first
semi-autonomous mission on 13 February 2026 under the Autonomy
Government Reference Architecture). On 20 April 2026, GA-ASI was
selected by NAVAIR PMA-281 for the Collaborative Autonomy Mission
Planning and Debrief (CAMP) project targeting a 2026 Fleet exercise
demonstration.
What is missing is the integrating authority — a single Air Force
Life Cycle Management Center program that pulls the six axes into a
coherent MQ-9B Block upgrade with a named configuration baseline, a
flight-test schedule, and a fleet retrofit timeline. Retired Brig. Gen.
Houston Cantwell and Douglas Birkey argued in Air & Space Forces Magazine
on 20 April 2026 that the Air Force should backfill Epic Fury's combat
losses with advanced MQ-9Bs rather than continue drawdown to 140
aircraft by 2035 — "the MQ-9B production line is hot, so the time to buy
is now." The correct version of that argument is sharper: buying more
of the same MQ-9A Block 5 configuration re-runs the Iran attrition
curve. Buying MQ-9B airframes with the six-axis evolution baseline makes
the Reaper the platform the Pacific campaign actually requires.
A Hypothetical 2028 Pacific Mission
Three MQ-9B SkyGuardians launch from dispersed Agile Combat
Employment sites in the First Island Chain under single-operator
control, autonomous takeoff and land. LAC-12 pods come online at
altitude, linking through Tranche 1 to Mission Delta 9 at Vandenberg.
Quantum MagNav holds position against pervasive PLA GPS spoofing inside
the A2/AD bubble. SkyGuardian A transits to a 200-nm hold point east of
the Strait, Lynx running CCD on coastal TEL hide sites at 3-hour
intervals; SWIR cross-cues the moment a plume is detected. Track data
pushes through the optical mesh to an SM-6-equipped destroyer in the
Philippine Sea and to HBTSS for handoff to Glide Phase Interceptor
fire-control. SkyGuardian B releases four PELEs at the ADIZ boundary to
geolocate emitters; PELE returns compressed ELINT over LAC-12.
SkyGuardian C, SeaGuardian variant, dispenses sonobuoys over a known PLA
submarine transit lane; data is processed onboard and passed to a P-8
on combat air patrol 400 nm south via Link 16. At hour 28, all three
aircraft are relieved by the next wave, continuing unbroken coverage. No
crewed asset was exposed to a SAM ring. No GPS-jammed Reaper lost lock.
The kill chain closed at the speed of light.
The Choice
Every mid-life platform faces this decision. The F-16 chose to evolve
through a half-dozen block upgrades and is still the most-produced
Western fighter in service. The B-52 chose to evolve through a series of
engine and avionics programs and will fly into the 2050s. The P-3 chose
not to, and was replaced. The MQ-9 is at that decision point now. It
can be allowed to decline into an increasingly specialized
counterterrorism asset, drawn down to 140 airframes and quietly retired
behind the CCA curtain by the mid-2030s. Or it can be evolved —
rigorously, on a program of record, across the six axes this article
describes — into the distributed sensor-and-shooter node the Pacific
campaign actually requires.
The argument for the latter is that every element is demonstrated.
The ALCoS and LINCS air-to-space laser links are closed. The SDA Tranche
1 mesh is operational. The quantum MagNav is flying. The M-code EGI is
certified. The PELE is announced. The JASSM/LRASM/JSM integration is
active engineering. The F-22/MQ-20, F-35/CCA, and P-8/SeaGuardian
teaming demonstrations are in the books. The MQ-9B production line is
hot. The Indo-Pacific sensor web is expanding month by month across
allies.
Epic Fury, read closely, is not the epitaph of the MQ-9. It is the
calibration trial — the brutal field test that identified which
architectural assumptions no longer hold. The ones that held —
endurance, modularity, open architecture, production maturity, allied
interoperability, the specific SWaP envelope that made ALCoS possible
and that LAC-12 now exploits — are precisely the ones that matter for
tomorrow. Evolution, not retirement, is the defensible programmatic
path. The aircraft designed around Honeywell triple redundancy and a
Ku-band pipe to fight the last war can be evolved into the aircraft
designed around laser links, quantum sensors, launched effects, and
standoff missiles to fight the next one. The window to decide is
measured in the budget cycles between now and 2028. The aircraft to
evolve are on the ramp.
"Seabirds achieve unbelievably efficient
navigation, even from places they have not previously visited, and do so
without the help of satellites." — Dr. Ollie Padget, University of Liverpool, 23 March 2026
The seabird project at York and Liverpool is the deeper frame.
Evolution worked not by building one exquisite compass but by weighting
many ordinary cues. The Pacific campaign that is coming will be won by
the same principle — distributed sensors, layered links, redundant
navigation references, human commanders routing authority through
autonomous sub-elements, and an architecture that degrades gracefully
under attack rather than collapsing. The MQ-9B, evolved, is one of those
cues. Not the center of the architecture. One node in it. That is a
defensible, funded, achievable future. It is also the only one on offer
that does not require waiting for the next airframe to fix a problem the
services have today.
Q-CTRL et al. "Quantum-assured magnetic navigation achieves
positioning accuracy better than a strategic-grade INS in airborne and
ground-based field trials." arXiv:2504.08167, Apr 2025. https://arxiv.org/html/2504.08167v1
Gnadt, A.R. et al. "Signal Enhancement for Magnetic Navigation
Challenge Problem" (USAF/MIT MagNav Challenge; Cessna Grand Caravan
platform; five scalar cesium magnetometers, four fluxgates).
arXiv:2007.12158. https://arxiv.org/abs/2007.12158
Physics-Informed Calibration of Aeromagnetic Compensation using
Liquid Time-Constant Networks. arXiv:2401.09631, Jan 2024 (58–64%
compensation error reduction vs Tolles-Lawson baseline). https://arxiv.org/html/2401.09631v1
"Airborne Magnetic Anomaly Navigation with
Neural-Network-Augmented Online Calibration" (cold-start EKF + NN, F-16 /
MagNav Challenge dataset). arXiv:2603.08265, Mar 2026. https://arxiv.org/abs/2603.08265
Canciani, A. and Raquet, J. "Airborne Magnetic Anomaly
Navigation." IEEE Transactions on Aerospace and Electronic Systems
53(1): 67–80 (2017) — Tolles-Lawson baseline reference for the
literature.
U.S. Patent 4,755,904. "Lightning protection system for
conductive composite material structure" (foraminous metal / copper mesh
embedded in outer laminate; bonding to engine/ground-plane). https://patents.justia.com/patent/4755904
Airframer. "General Atomics MQ-9 program supplier guide" (GA-ASI
completes full-scale fatigue test on MQ-9B, 17 Nov 2025; El Mirage
expansion 22 Jan 2026; GA-ASI/Calidus MOU for MQ-9B co-production, 20
Jan 2026). https://www.airframer.com/aircraft_detail.html?model=Predator_B
"A Multi-Industry Perspective to Composite Repairs." Applied
Composite Materials, Jun 2025 — Commercial Aircraft Composite Repair
Committee (CACRC, founded 1991); bonded repair size limits on 787
primary structure; NDT limitations for adhesive bond strength. https://link.springer.com/article/10.1007/s10443-025-10351-3
Aviation Maintenance Magazine. "Aviation Composite Repair: An
Essential Core Competency" (Evans Composites, HAECO Composite Services,
Vallair — industry concentration into vertically-integrated specialty
houses), Oct 2025. https://avm-mag.com/aviation-composite-repair-an-essential-core-competency
Comtek Advanced Structures. Corporate capability description
(Latécoère subsidiary, AMO and DAO credentials, composite primary and
secondary structure repair beyond SRM limits). https://www.comtekadvanced.com/
San Antonio Report. "San Antonio's Boeing facility gets boost
from upgrading B-52s" — Port San Antonio (formerly Kelly AFB) B-52 radar
modernization; Boeing's acknowledgment that the B-52 "was first
designed with pencils and paper in the 1950s"; $2.8 billion
modernization program. https://sanantonioreport.org/b52s-boeing-port-san-antonio-upgrade-air-force/