The F-35′s Air-to-Air Capability Controversy

F-35A
F-35A test flight
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The $300+ billion, multi-national F-35 Joint Strike Fighter program is the largest single military program in history. It’s also reaching a critical nexus. In order to keep costs under control and justify the industrial ramp up underway, participating countries need to sign order agreements soon. The problem is that the F-35 is not a proven fighter design, with a demonstrated baseline of performance in service. It’s a developmental aircraft in the early middle of its test program, which is now scheduled to continue until 2018 or even 2019.

As one might expect, this status makes the F-35 a controversial long-term bet in many of the program’s member countries. Costs aren’t certain, numbers ordered are slipping in many countries, and timelines aren’t certain after numerous schedule delays. With combat testing still a year or 2 away, even operational performance isn’t certain. That’s especially consequential for air forces that expect to field the F-35 as their only fighter.

September 2008 featured a very public set of controversies around the F-35′s air combat performance. Many partner countries were beginning to make decisions about their long-term needs, so the altercation in Australia became a controversy with implications, and responses, that reached well beyond that continent’s shores. The RAND study that triggered it didn’t specifically address the F-35, but it does have implications for the F-35′s projected performance – and for the heart of the USAF’s current fighter force concept.

This article takes a much closer look at the RAND Pacific Vision study, while bringing in other opinions, analyses, and subsequent developments. Understanding the F-35′s real air superiority potential and weaknesses, and their implications for partner nation participation, has only grown in importance since 2008. Let us begin…

F-35: September 2008′s Australian Altercation

F-111 and F-18 RAAF
The current roster
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On Sept 11/08, The Sydney Morning Herald reported that Australian Defence Minister Joel Fitzgibbon had asked for a full report from Australia’s DoD, in response to public reports that a classified computer simulation of an attack by Russian-built SU-30 family aircraft on a mixed fleet of F-35As, Super Hornets and F-22s, had resulted in success for the Russian aircraft. Fitzgibbon, who questioned the strategic logic behind Australia’s plans for an F-35/ F-18F fighter fleet while in opposition, asked for an Australian Department of Defence review, and added that:

“I’m determined not to sign on the dotted line on the JSF until I am absolutely certain it’s capable of delivering the capability it promises and that capability can be delivered on time and on budget.”

On Sept 12/08, Australia’s opposition Liberal Party waded into the fray in support of its previous decision to buy the F-35A. It asked the new minister to release the results of the recent Air Combat Capability Review, and get on with his decision.

Even so, the timing of this contretemps could not have been worse from Lockheed Martin’s perspective. Just 3 days earlier, the left-wing American Center for Defense Information had released “Joint Strike Fighter: The Latest Hotspot in the U.S. Defense Meltdown.” Its commentary echoed some items that were in the RAND study, though those items were not the study’s focus. Lockheed Martin and the USAF soon countered, and the controversy became an international issue.

In order to really understand that controversy, one must first look at what the RAND report did and did not say. Fortunately, that is now possible, thanks to a leaked and posted copy. The subsequent controversies involving CDI, Lockheed Martin, et. al. will make more sense in this context. Once the various claims and counter-claims are clear, it becomes possible to evaluate their strengths and gaps, then match that to potential impacts on the larger F-35 program, and its sales.

Australian Altercation: RAND’s Pacific Vision Study

CORP_RAND_Logo.jpg

On Sept 25/08, the RAND Corporation stepped in with a statement of their own concerning the August 2008 Pacific Vision simulation performed under its wide-ranging Project Air Force mandate:

“Recently, articles have appeared in the Australian press with assertions regarding a war game in which analysts from the RAND Corporation were involved. Those reports are not accurate. RAND did not present any analysis at the war game relating to the performance of the F-35 Joint Strike Fighter, nor did the game attempt detailed adjudication of air-to-air combat. Neither the game nor the assessments by RAND in support of the game undertook any comparison of the fighting qualities of particular fighter aircraft”

That last assertion is true. On the other hand, DID managed to obtain a copy of the RAND Power Point briefing. When the full briefing is read, RAND’s study does have implications for the F-35. They are decidedly mixed.

F-35A JSF & F-22A Raptor
F-35A & F-22A,
Eglin AFB
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RAND is correct that their study did not attempt any adjudication of air combat. Indeed, its assumptions of perfect missile attack by American F-22 fighters, and similarly perfect missile defense by F-22s, were designed to remove this very issue from the equation. When F-35s did participate in the analysis, the full range of “missile kill probability” figures from 1% to 100% were offered as “what if” tools, without making predictions or distinctions based on either side’s aircraft.

The core problem in Pacific Vision 2008 was that even an invulnerable American fighter force ran out of missiles before it ran out of targets, at any number below 50% of missile firings resulting in kills. Whereupon the remaining Chinese fighters would destroy the American tankers and AWACS aircraft, guaranteeing that the USAF’s F-22As would run out of fuel and crash before they could return to Guam.

To reiterate: RAND’s core conclusion is not about specific fighter performance. It’s about the theoretical limits of better performance under adverse basing and logistics conditions. RAND’s Project Air Force argues, persuasively, that based on history and current trends, numbers still matter – and so does the “Lanchester square.” That’s the theory under which the combat performance of an outnumbered combatant must be the square of the outnumbering ratio (outnumbered 3:1 must be 9x better, etc.) just to stay even.

Or, as the oft-repeated Cold War era saying goes, “quantity has a quality all its own.”

F-35: Air to Air Analyses

Hostile Trends

F-22A fires AMRAAM
AIM-120C from F-22A
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The belief in quantity could be seen as a point in the F-35′s favor, when comparing it to its implicit F-22 as a rival for USAF dollars. Even so, it’s prudent to note that the RAND study revolved around total missiles carried, and the F-35′s internal capacity will be no larger than half of the F-22′s (no more than 4 missiles, vs. 8 in the F-22A). Equivalent air-air missile capacity at each aircraft’s maximum stealth configuration thus requires at least twice as many F-35s as F-22s. Plus the cost of the extra aerial tankers and other infrastructure required for long-range missions.

The RAND study also spends a great deal of time on the core American assumptions concerning “beyond visual range” air to air combat, and the current and future capabilities of SU-30 family aircraft. The implications of its examination do affect the F-35′s fighting qualities – and they will be significant to some of the plane’s potential customers.

RAND’s discussion begins by predicting poorer beyond visual range missile kill performance than current models suggest when facing capable enemy aircraft, observing that BVR missile kills since the 1990s generally involved poorly-equipped targets. It also notes the steep rise and then drop in modern infrared missile performance, as countermeasures improved.

Meanwhile, key radar advances are already deployed in the most advanced Russian surface-to-air missile systems, and existing IRST (infra-red scan and track) systems deployed on advanced Russian and European fighters are extending enemy detection ranges against radar-stealthy aircraft. Fighter radar pick-up capability of up to 25 nautical miles by 2020 is proposed against even ultra-stealthy aircraft like the F-22, coupled with IRST ability to identify AMRAAM missile firings and less infrared-stealthy aircraft at 50 nautical miles or more.

The F-35′s lower infrared and radar stealth levels mean that these advances will affect it more than they’ll affect the F-22. Especially if one assumes a fighter aircraft whose prime in-service period stretches to 2050.

The clear implication of the RAND study is that the F-35 is very likely to wind up facing many more “up close and personal” opponents than its proponents suggest, while dealing with effective beyond-visual-range infrared-guided missiles as an added complication. Unlike the F-22, the F-35 is described as “double inferior” to modern SU-30 family fighters within visual range combat; thrust and wing loading issues are summed up in one RAND background slide as “can’t [out]turn, can’t [out]climb, can’t [out]run.”

The Argument Room

F-35A Armed
F-35A, armed test
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Some of these criticisms were echoed in the left-wing American Center for Defense Information’s Sept 8/08 briefing “Joint Strike Fighter: The Latest Hotspot in the U.S. Defense Meltdown.” This analysis by Pierre M. Spey, a key member of the F-16 and A-10 design teams, cast sharp doubt on the F-35′s capabilities:

“Even without new problems, the F-35 is a ‘dog.’ If one accepts every performance promise the DoD currently makes for the aircraft, the F-35 will be: “Overweight and underpowered: at 49,500 lb (22,450kg) air-to-air take-off weight with an engine rated at 42,000 lb of thrust, it will be a significant step backward in thrust-to-weight ratio for a new fighter… [F-35A and F-35B variants] will have a ‘wing-loading’ of 108 lb per square foot… less manoeuvrable than the appallingly vulnerable F-105 ‘Lead Sled’ that got wiped out over North Vietnam… payload of only two 2,000 lb bombs in its bomb bay… With more bombs carried under its wings, the F-35 instantly becomes ‘non-stealthy’ and the DoD does not plan to seriously test it in this configuration for years. As a ‘close air support’… too fast to see the tactical targets it is shooting at; too delicate and flammable to withstand ground fire; and it lacks the payload and especially the endurance to loiter usefully over US forces for sustained periods… What the USAF will not tell you is that ‘stealthy’ aircraft are quite detectable by radar; it is simply a question of the type of radar and its angle relative to the aircraft… As for the highly complex electronics to attack targets in the air, the F-35, like the F-22 before it, has mortgaged its success on a hypothetical vision of ultra-long range, radar-based air-to-air combat that has fallen on its face many times in real air war. The F-35′s air-to-ground electronics promise little more than slicker command and control for the use of existing munitions.”

On Sept 18/08, Lockheed Martin fired back in “F-35: Setting the Record Straight.” It takes direct aim at both the Australian press reports, and the CDI article, noting that external weapons clearance is indeed part of the F-35′s current test program. Lockheed Martin added that:

“…The Air Force’s standard air-to-air engagement analysis model, also used by allied air forces to assess air-combat performance, pitted the 5th generation F-35 against all advanced 4th generation fighters in a variety of simulated scenarios… In all F-35 Program Office and U.S. Air Force air-to-air combat effectiveness analysis to date, the F-35 enjoys a significant Combat Loss Exchange Ratio advantage over the current and future air-to-air threats, to include Sukhois… In stealth combat configuration, the F-35 aerodynamically outperforms all other combat-configured 4th generation aircraft in top-end speed, loiter, subsonic acceleration and combat radius. This allows unprecedented “see/shoot first” and combat radius advantages.

The high thrust-to-weight ratios of the lightweight fighter program Wheeler/Sprey recall from 30 years ago did not take into consideration combat-range fuel, sensors or armament… We do consider all of this in today’s fighters…

…Simply put, advanced stealth and sensor fusion allow the F-35 pilot to see, target and destroy the adversary and strategic targets in a very high surface-to-air threat scenario, and deal with air threats intent on denying access — all before the F-35 is ever detected, then return safely to do it again.”

Note that Lockheed Martin’s release does not address infrared stealth against modern IRST (infra-red scan and track) air to air systems, which are present on advanced European and Russian fighters. The F-35 will use a clever system that circulates fuel near the aircraft skin to remove some frictional heat, but it still has a 40,000 pound thrust turbofan in the back, and Russian designs already have ranges from 50 km (OLS35, head on) to 90 km (OLS35, rear). Nor does it make any claims concerning superior maneuverability against thrust-vectoring opponents like Russia’s MiG-29OVT and the most modern members of the SU-30 family, or canard-equipped “4.5 generation” aircraft like the Dassault Rafale, EADS Eurofighter, or Saab’s Gripen.

Can these statements be reconciled – and if not, which of them are incorrect? Some of the F-35 program’s success could hinge on the answers to those questions.

AIR F-35 Left Wingover Rear View
F-35A #AA-1
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Part of the problem is that both the CDI’s analysis, and Lockheed Martin’s reply, are incomplete.

Spey has undertaken a similar analysis of the F-22A Raptor for CDI, but aircraft pilots have said that his analysis in key areas like maneuverability is poorly done, and does not match provable reality. Spey’s wing-loading model claimed superiority for the F-15, when the F-22 has significantly better instantaneous and sustained turning capabilities (28 degrees sustained, vs. 21/15-16 degrees per second instantaneous/ sustained). This justifies strong caution in accepting Spey’s F-35 analysis, and Lockheed Martin’s reply offers additional reasons for doubt. In fairness to Spey, it should also be said that combat experience with his A-10 aircraft in Afghanistan etc. does back up his contentions concerning the limitations of fast jets, and the capabilities required for close air support.

The F-35′s problem is that concrete reasons could be advanced to explain why Spey’s F-22 aerodynamic analysis parameters were wrong, such as the Raptor’s thrust vectoring and controllable tail surfaces to offset Spey’s unidimensional wing loading analysis, the tactical implications of having the ability to cruise above Mach 1 without afterburners, and stealth that has defeated AWACS aircraft and worked against international fighter pilots even at relatively short ranges. F-22 pilots have also racked up incredibly lopsided kill ratios in American and international exercises, far in excess of “normal” performance for new aircraft, that back up their pilots’ performance claims.

This is all much harder to do for the F-35, which remains a developmental aircraft and lacks key aerodynamic features like combat thrust vectoring (Harrier, SU-30 family, MiG-29OVT, F-22A), canards for fast “point and shoot” maneuvers with high off-boresight short-range missiles (some SU-30 family, Rafale, Eurofighter, Gripen), or loaded supersonic cruise (F-22A). The F-35 has also been designed from the outset to feature less stealth than the F-22A, though it will be stealthier than contemporary 4.5 generation European and Russian aircraft. Aircraft intake size and hence volume are set unless the aircraft is redesigned, and wing size, angle and loading can all be observed.

Indra Dhanush: SU-30MKI, Eurofighter & Tornado-F3
@Indra Dhanush
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The F-35′s explicit design goal has been stated as being the F-16′s equal in in air to air combat, at a time when the F-16′s future ability to survive in that arena is questioned. The question naturally arises: what special features give the F-35 a unique ability to prevail against the kind of advanced, upgraded 4.5 generation and better fighters that it can be expected to face between its induction, and a likely out of service date around 2050 or later?

Classified simulations whose assumptions are shielded from the public may indeed demonstrate the attested results, but their foundations are outside any public scrutiny, and amount to a claim that must be taken on faith. That may not be very convincing in the political sphere. Especially since models of this type have been very wrong before, due to the well-known phenomenon of incorrect or missing assumptions producing results that don’t match the test of battle.

The F-35 does have the equivalent of a Sniper ATP reconnaissance and targeting pod built in, and experience on the front lines indicates that its presence goes significantly beyond just “slicker command and control for the use of existing munitions.” That addresses an important component of the F-35′s overall rationale – but it does not address the air to air dimension.

Hence Lockheed Martin’s limited success in the public relations sphere. Aviation Week’s veteran journalist Bill Sweetman, for instance, greeted Lockheed Martin’s September 2008 air superiority claims with a reaction best described as incredulity:

“Moreover, it’s made just as Graham Warwick reports (subscription) that Maj. Richard Koch, chief of USAF Air Combat Command’s advanced air dominance branch, stated last week: “I wake up in a cold sweat at the thought of the F-35 going in with only two air-dominance weapons.” There is surely a universe where these two statements are compatible, but we don’t live there… If the F-35 can really do all that, why did the USAF spend billions on supercruise, rear-aspect stealth and supermaneuverability (the reason for 2D vectoring nozzles) for the F-22? And does this mean that the all-aspect/wideband LO tech on the B-2 and X-47B UCAS is superfluous?”

DAS Plane

F-35 EO DAS
(click to view video)

In a follow-on October 2008 article however, Sweetman described a possible air-to-air feature that may offer a partial explanation for Lockheed Martin’s claims. As RAND noted, improvements in countermeasures have affected infrared missile kill probabilities, and this system has yet to be tested in realistic combat scenarios involving multi-spectral flares, etc. With that said:

“[The F-35's AN/AAQ-37 Electro-Optical Distributed Aperture System] comprises six fixed, wide-angle infrared cameras that constantly image the entire sphere around the F-35… and one of its functions is to provide imagery to the VSI helmet-mounted display… one of the DAS’ most interesting capabilities is that it can constantly track every aircraft in the sky, out to its maximum range… covers the within-visual-range envelope… it stares, never looking away from any target, and it has optical accuracy, with megapixel-class resolution… Moreover, DAS is expected to track with enough accuracy and tenacity to permit a safe high-off-boresight, lock-on-after-launch (LOAL) missile shot with any datalink-equipped missile. Indeed, Northrop Grumman’s DAS business development leader, Pete Bartos – who was part of the initial USAF JSF requirements team – says that this was basic to the F-35 design and the reason that it did not need maneuverability similar to the F-22. Rather than entering a turning fight at the merge, the F-35 barrels through and takes an over-the-shoulder defensive shot. As a Northrop Grumman video puts it, “maneuvering is irrelevant”.”

This feature would also explain the F-35′s 1960s-style cockpit with its limited rear visibility. Despite its stealth benefits, analysts like Pierre Spey have seen it as a retrograde step – one that disregards the air-to-air combat lessons which drove the bubble cockpits on America’s “teen series” (F-14, F-15, F-16, F/A-18) fighters.

The HMDS helmet-mounted display is supposed to solve that problem electronically, by drawing on the plane’s sensors. Using HMDS and DAS, a pilot looking down can even “look right through” the floor! Unfortunately, HMDS is one of the fighter’s most problematic components as of 2013.

F-35: The Air-Air Controversy and Program Success

F-35B STOVL Landing
X-35B STOVL
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Which leaves many a defense ministry or and politician asking the question, as they prepare to place a big bet on their future air force: “Will all of this work?”

Ultimately, solid proof comes from use in combat against peer opponents. Israel’s nuclear program removed that perennial testing ground, by ending the consistent string of conventional wars that used to be the globe’s top source for that kind of information. Nor has any other source for that kind of peer conflict data emerged since the 1990s. If the F-35 lacks that kind of backing, well, so do all of its competitors.

These days, an imperfect but acceptable substitute may be available via performance in multinational exercises like Red Flag or Indra Dhanush, where some of the opponents will have less institutional incentive to soft-pedal comparative performance claims in the name of a united organizational front.

As it happens, that air to air dimension will not be a priority for every customer.

Some customers may be quite satisfied with a manned fighter that offers good international/NATO commonality, the ability to perform basic airspace sovereignty duties, good survivability against medium to advanced air defenses if encountered, off the shelf surveillance and targeting capabilities that exceed all other contemporary fighters, and the ability to carry enough weapons to support international missions against opponents up to the level of Serbia or al-Qaeda and the Taliban. For those countries, even an F-35 that matched Spey’s characterization might well suffice.

Questions of industrial benefits and costs, rather than air to air capabilities, will dominate fighter replacement discussions in those countries. The F-35 program has already seen a 54.4% increase in overall program costs per aircraft delivered from 2001 to the present day, and the US GAO believes that another 14.5% rise to about $327 billion for 2,456 American fighters could still lie ahead. If the GAO is correct, it would place the fully-loaded program cost of each F-35 at $137 million. That price is not at all the same as the “flyway cost” of buying an individual aircraft, but it does affect program partners if the USA isn’t prepared to bear those additional program costs alone. Or if rising costs force the USA to slash its own procurement numbers yet again, a move that would affect the aircraft’s production economies of scale and learning curves.

Budgetary and industrial concerns will always be part of the debate, but some customers may also have stricter performance requirements to deal with.

If a country needs aircraft to operate from small aircraft carriers or amphibious assault LHDs, the AV-8 Harrier’s age and projected phase-out plans will make the F-35B STOVL (Short Take Off, Vertical Landing) their only non-Russian option. Customers in this category already include the US Marine Corps, Italy, Spain, and Thailand. Australia and South Korea are both fielding ships that could be used to host STOVL fighter jets if they wished, and the number of countries in that category seems set to grow as LHD amphibious assault ships become more popular. Very large LHDs, or small carriers equipped with ski-jumps, may also allow some competition from the less flexible STOBAR (Short Take Off But Assisted Recovery) MiG-29K, which India’s navy plans to induct by 2011 or so. For those customers, the choice boils down to having fighter jet launch capability from those platforms – or not.

F-35C
US Navy F-35C
(click to view full)

On the flip side, if maintaining regional or local air superiority is a priority mission for any replacement fighter, then aerial performance against enemy aircraft becomes extremely important. This is certainly true for the US Navy’s carrier fleet, for Australia’s RAAF, for Israel’s IAF, and to a lesser extent for the future British Navy. When addressing these customers, Lockheed Martin must depend on political inertia or limited export choices – or advance plausible, non-classified rationales that explain why its F-35s will perform as an air superiority fighter. Australia may have been the first potential customer to raise the issue this openly in the political sphere; it is unlikely to be the last.

What’s common to every potential F-35 customer, of course, is the time factor. Competitively tested performance, and firm costs, are both some years away. Yet many defense departments around the world will need to make decisions before that evidence becomes available. Hence the current political conundrums in country after country, and the tension that inevitably surrounds any program of this size before key commitments are made.

As Aviation Week’s Bill Sweetman put it in an August 2008 article:

“If the JSF program succeeds in locking up its international partners, the project could be within reach of its goal of an F-16-like, mid-four-digit production run… But if JSF falls short of its goals – as almost every major military aircraft program has in the past 25 years – it will throw the re-equipment plans of a dozen air arms into disarray.”

Postscripts and Updates

NGC re: APG-81 radar
click for video

Feb 7/13: Claims & Controversy. Flight International is still doing test pilot interviews, and also talking to Lockheed Martin. The resulting collision of views is interesting. Lockheed test pilot Billy Flynn is writing the book on F-35 flight envelope expansion, and has flown Eurofighters, F-16s, and NASA’s thrust-vectoring F-16s and F/A-18s. He opens the debate with the provocative view that the F-35 is superior to existing 4+ generation fighters like Eurofighter’s Typhoon etc. on just about every metric – but some of his fellows in the test pilots fraternity are a bit dubious. To help readers keep score, here are the key contentions and responses:

F-35 air-to-air arguments
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Jan 30/13: Pilot Views. Flight International interviews both experienced pilots and Lockheed Martin personnel, in the wake of the performance downgrades announced by DOT&E’s 2012 report. Those downgrades affect survivability against incoming air defense missiles, where maneuvering performance is critical when attempting to break their guidance lock. Nor are they especially helpful in combat against aircraft whose maximum and sustained turn performance heavily outclass it.

On the “bright” side, the F-35 is said to have good instantaneous turn performance and good high (50 degree limit) angle of attack performance, comparable to a Boeing F/A-18 Hornet. Lockheed Martin business director and former combat pilot Steve O’Bryan also cites the F-35′s performance at high altitude, claiming that it can outclass other Gen 4/4+ fighters “that [he's] familiar with” when operating “clean” and relying on its weapon bays.

That may be true, but many air combat engagements quickly descend from high altitude and into lower altitudes and speeds, as participants bleed energy in turns and maneuvers. Energy is life, and acceleration matters. As for the F/A-18A-D Hornet, it’s a good but not great dogfighter by 1990s standards, whose defining strength is its performance at slow speeds.

All fighters have limitations, and fighting to your plane’s strengths is a big component of good airmanship. What’s concerning is the apparent number and extent of the F-35′s kinetic weaknesses, and the structural difficulty of fixing them. The net tactical effect is that pilots will be forced to depend even more heavily on electronics like the EO DAS and APG-81 radars, and on a stealth profile that’s less effective and more variable than the F-22A’s. Flight International.

F-35C with AIM-9X
F-35C, armed
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Jan 13/13: Testing. The Pentagon’s Department of Operational Test & Evaluation submits its 2012 report, which includes 18 pages covering the F-35. The fleet continues to work through significant technical challenges, which isn’t unusual. What is unusual is the steady stream of deliveries that will have to be fixed later, in order to address mechanical and structural problems found during testing. From an air-to-air point of view, 2 issues deserve special mention.

One issue is weight. The F-35 was designed with little margin for weight growth, but new capabilities and fixes for testing issues often add weight. Weight growth above designated limits directly affects aerial performance, and at some point, weight dilemmas can become a lose/lose proposition. One frequent consequence is higher costs, for example, as very expensive but lightweight materials are used to save an extra pound here and there. Another consequence is reduced performance, as seen in the F-35B’s drop to 7.0 maximum Gs after its aggressive weight reduction effort. A third consequence involves ruggedness and survivability, as seen by the fleet-wide problem created by saving just 11 pounds in all variants. Without fuelstatic flow fuses and Polyalphaolefin (PAO) coolant shutoff valves, DOT&E estimates that these flammable substances make the F-35 25% less likely to survive enemy fire.

The second issue that deserves especial mention is that key aerial combat standards have been lowered, following initial tests. All F-35s will sit at 5.0g or less sustained turn performance – a figure that places them in a class with 1960s era planes like the F-5 or F-4 Phantom, instead of modern designs like the F-16. Acceleration is also poorer, compared to a reference F-16C Block 50 with AMRAAM missiles on its wingtips zooming from Mach 0.8 to Mach 1.2.

The USAF’s F-35A dropped the most, from an expected 5.3g – 4.6g in sustained turns. Acceleration will take 8 seconds longer than the F-16.

The STOVL F-35B dropped from 5.0g to just 4.5g, and its engine is weaker in straight flight performance, in exchange for increased thrust during vertical landings. Its acceleration takes 16 seconds longer than the F-16.

The Navy’s large-winged F-35C did best in turning, with a slight drop from 5.1g – 5.0g, but trans-sonic acceleration was abysmal at 43 seconds longer. DOT&E report [PDF] | Lockheed Martin re: 2012 testing | Reuters | TIME magazine. | Washington Post.

March 20/12: Australia. Former Australian research scientist and defense analyst Dr. Dennis Jensen, MP [Liberal - Tangney, near Perth] makes a point of addressing the F-35′s air superiority capabilities:

“ADF [Australian Defence Forces] still contend that the overall capability of the JSF is superior and that it will defeat all discernible threats…. To get a handle on the assertions made by Defence, I worked through a step by step process of an 8 versus 8 combat. It was evident that this process was not going to end well for the JSF, so the “we are getting into classified areas” get out of jail free card was pulled. I can confirm that we were not even close to classified data.

….JSF and USAF analysts stated that against Su-27 and MiG-29 fighters the Raptor had a kill ration of 30 to 1 and the JSF 3 to 1…. Against aircraft 30 years newer, such as Su-35S, PAK-FA and the Chinese J-20, and you can imagine the results are likely to be very different…. AVM [Air Vice-Marshal] Osley advised that the JSF has some 650 ways to detect and avoid such threats…. if a JSF has to leave airspace because it detects the presence of Su-35Ss, PAK-FAs or J-20s that it cannot defeat, then the enemy wins airspace-dominance without firing a shot.”

Oct 28/08: Former Australian research scientist and defense analyst Dr. Dennis Jensen, MP [Liberal - Tangney], reveals that respected senior analyst and Pacific Vision 2008 lead John Stillion has left RAND. In a speech to Parliament, he says the departure raises “deeply disturbing” questions, adding that:

“There are suggestions in some quarters that he was dismissed over the document and that his removal was ordered by the US military.”

Official release.

Additional Readings

The F-35 Family

Argument Room, Redux

“Federal Member for Tangney Dennis Jensen revealed John Stillion, a respected senior analyst with RAND’s Project Air Force, had abruptly left the organisation and that there were suggestions he had been dismissed over the [Pacific Vision 2008] report.”

Other Planes & Perspectives

Categories: Australia & S. Pacific, Britain/U.K., Budgets, Fighters & Attack, Issues - Political, Lobbying, Lockheed Martin, T&C - RAND Corp., Transformation, USA

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