The
alternate AMCA Part 1. Prof. Prodyut
Das
Introduction
The Americans fought the air war over Vietnam with two
technically superb warhorses the F4 Phantom and the F105 Thunderchief. These
aircraft represented what the most powerful and innovative Aircraft Industry in
the world could develop. 761 of the former and 382 of the latter were lost over
a seven-year period in their attempts to “bomb North Vietnam back to the stone
age” falling to a low-cost Air Defence system.
The Americans appear
to have one of the most data-based process of aircraft specification fixing
that we know of and yet had the Americans had included a good Astrologer in
their processes they may have got the prediction to ignore the above to focus
and expedite the aeronautically mundane Grumman A6 Intruder, the North American
OV 10 and the Republic A 10. These aircraft were more suited to the scenario.
For example, the Americans, engaged as they were in destroying low value
targets defended by low value defences- dense AAA, obsolete SAMs and obsolescent
interceptors in cloudy Vietnam weather supersonic capability was actually a
penalty; the nocturnal A6 Intruder, subsonic but with advanced night attack/
bad weather capability, would have nullified much of the formidable Vietnamese
AAA or the daylight only MiGs which were the main killers. Similarly for the
other two types. The Americans would not have won the war but they would have
caused much greater casualties at much lower costs and it is an unknown what
that may have led to.
So why did the Americans end up with the wrong/ less appropriate
war planes for the type of war they actually fought? There are complex reasons
but briefly it can be put down to the following:
i)
Weapons specifications must stem from long term political
aims. Clausewitz
said War is an extension of national aims by other means then the corollary
to Clausewitz is: the nation’s
war plans, strategic policy and aims must be clearly spelled out by the Political
policy makers to the Military in “inter-pares” planning. The ability of the
Soviet Union to get well-suited weapons at low prices came because its weapons
development was tied to national political aims. It is very probable that the present Chinese
“challenge” today had its foundations to political ambitions elucidated decades
ago. The American specifications which appears to be subject of much copying-are
much too general or “all- rounder” which is always difficult to engineer.
ii)
The process of fixing specifications is something like
the four blind men and the elephant. The person
who sets up the specifications knows exactly what he wants- he has been working
in that line for thirty years. However he does not know how to engineer it what are
the trade- offs and he does not pay for it; he also does not know when and what
war he will be asked to fight and the political stand then will be. It is one
of those unusual cases where the customer knows what he wants but does not pay
for it; The Engineer is motivated to get the project “at all costs” and will
put up with a fair amount of ordure/tell lies/sell dreams to land the order.
In the West this “unworkable” situation usually works because most
stakeholders usually have knowledge-almost to the “hobbyist” or “fanatique”
level about each other areas, they (usually!)
have a greater degree of respect for each other competences. The “owner”
i.e., the financier, is keenly interested in quick outcomes and, of course, the
industry moves very rapidly to hardware-three to four years being the norm.
iii)
Futurology. Fixing relevant
specifications is one of futurology. The process begins to delve into the
unknown as e.g., the USAF in Vietnam. Faced with the unknown the protagonists
do what the schoolboys do when facing a question paper which they do not know-
they cheat and copy from each other which is why many specifications look like
a copy of the other.
iv)
Over specification. The customer,
because of the reasons above set up unattainable specifications. The recent New
Delhi story goes of a specification for an assault rifle which could mount all
sorts of additional equipment but it was found that there was no space for the
trigger. After much redesign space was found for the trigger but there was
no space at all for the trigger guard which of course rendered the super
rifle useless and specifications was scrapped after wasting much time. Over specification is a pity because often very
useful specifications can come from original thinking.
v)
The topic of the haphazard dynamics of the struggle
between relevant versus glamourous specification, over conservatism and over
enthusiasm is vast; I cite just two examples as an appetizer.
vi)
Marketing and Auto suggestion: Since
weapons are designed to make a profit or generate influence the weapons wish to
have the largest possible market and so many influencers are employed. The Mach
2 requirement was a particular Western cold war era requirement that was
rendered obsolete in 1950s when nuclear weapons delivery was taken over by
ICBMs. Today it continues to be specified despite horrific complications in
terms of technology base required not to speak of costs. The rise and decline
of 5.62 mm as the main infantry weapon are another illustration that what is
generally accepted as necessary by the experts is often the result of
auto suggestion and marketing without any serious gaming of various
alternatives.
Unwillingness to venture into new concepts
The De Havilland Mosquito was a god send. It used a two- man crew to deliver, so the
story went, the same payload as eight man Flying Fortress but flew fifty m.p.h.
over much the same range. Its versatility was legendary. It used non- strategic
materials and skills for its production and yet the RAF never had as many as
they wanted because when proposed it was the “experts” who tooth and
nail opposed to the idea of a “gun less” bomber which was central to the
concept. This opposition to “Freeman’s Folly”- Air Marshal Freeman was the lone
RAF supporter -delayed the service introduction of the aircraft by over two
years i.e., until 1942. The “experts” were not wrong; they were frightened/worried
that it was a “risky” concept-why take the blame/consequences if it fails; better
safe than sorry. Incidentally Original solutions ,as the Mosquito showed, can be remarkably more economical.
Insisting
that the general specification is the best bet: Closer
home, by 1956, it should have been clear- that a 4x30mm Aden armament and a
Mach 2.2 top speed was a pure Western Air Forces need to intercept the TU-16.
For India it was unnecessary, “thoughtless” and counterproductive. Tank
could have developed a smaller, longer range, more maneuverable and trouble-free
i.e., a “better” HF 24 if the specification had asked for 2X 30mm and a top
speed of say Mach 1.3 or so but the IAF specifications itself whilst “fashionable”,
actually played a role in the ultimate failure of the project e.g., the
insistence on Mach 2.2 scuttled the adoption of the Russian engine in 1964.
To sum the
specifications of the weapon must stem from scenarios evolving from identified
political objectives and the tendency to over specify have to checked against
the scenario laid down by the war aims. Specifying requirements without
specific political war aims is wasteful and we are missing out on other
alternatives. This proclivity for “standard specifications” is in part due to
the crippled structure of our weapons development Industry. Imported weapons
will for a short time be better but we don’t need arms to win spectacular
victories. It is sufficient to undermine the adversary’s confidence about the
final outcome.
The concept
of the alternate AMCA
The AMCA as
displayed has gradually matured into a fairly acceptable configuration but its
specifications, down to super cruise abilities appears to be a “cut and paste”
of comparable fifth generation fighters. In the process it has laid the seeds
of its own delays and non fulfilment. Is the AMCA specification as it stands
today the best way to achieve our political war aims? Reportedly we will
need a 120kN engine and we will not get it- even by the proposed
collaboration/s- a vendor’s reported reluctance to fulfil “buy back”
agreements regarding hypersonic tunnel and high-altitude test chambers should
be an indication of the “seller’s market” we are in. Should self-reliance in
powerplant be sacrificed to get super cruise? Super cruise is a deployment
rather than a combat need. Sacrifice it and see how much the development
burden reduces. Thel question to
answer is will a formidable state of the art warplane mired in uncontrollable development
delays deter aggression? There must be
options to explore something simpler and more achievable aircraft to hold the
fort? We don’t need to slash specifications drastically-only just those
which yield dividends.
We have to
get back to fundamentals. Some of the more important markers are:
1. Artificial
Intelligence and Smart weapons are changing the paradigm of weapons platform
design. The fundamental equation for combat success in mobile
warfare was Platform performance plus weapon plus intelligence equals
results. Increased “intelligence” of weapons i.e., smart weapons should
revolutionize and make flexible the design requirements of the platform. The
platform is no longer needed to bring the weapon to the enemy’s six o’ clock. This
flexibility is waiting to be exploited. Whilst manned aircraft will continue
into the foreseeable future their role will change from being an aiming platform
to more of a “carrier” or “transporter”. In case of technology
constraints as in India’s case, platforms of relatively modest energy or
“specific excess power” related performances coupled with intelligent weapons
can yield effective results specially as in our case when engines of the thrust
needed is not on the industry’s horizon.
2. Stealth
is specified without appreciation of its potentials. Stealth
is a substitute for speed. Given our weakness reference to engine
technology this does not appear to be sufficiently appreciated. There are also
contradictions. Stealth is specified with super cruise but stealth and super cruise
is:
i)
Contradictory because of kinetic heating but also the technology
required is heavy, expensive and not available to India. Super cruising is a
logistical rather than combat requirement. Can the specifications
authorities re-examine this as it would mean significant
simplifications in engine and airframe technologies?
ii)
The application of stealth will vary with the intelligence
of the weapon. The influence of stealth on platform design has changed because
of increasing intelligence” of the “weapon”. The F 119 went in for total or
Extreme Stealth-Radar, IR aural and visual because its weapons - LGB s were
“smart” but not “stand-off”. The aircraft had to overfly the target. The
F 35 is ignoring IR/Aural and Visual and it is probable that its radar
signature is not of the “one steel ball” kind of size of the F 117. In fact,
since Sokolnikoff’ s radar equation works both ways, the use of stand-
off weapons will reduce the level of stealth required in attacking a target.
This can again lead to major technical and cost reductions.
iii)
Stealth is most suitable for intruder/missile launcher
type of aircraft rather than on fighters.
A fighter requiring M2.2 will need approximately four
times the maximum power and yet at low levels the effect of afterburner on
speed is marginal. To ask for a M 2.2 capability and stealth-
when the country has yet to be developed is thus doubly illogical specially for
a critical weapon. We have to renegotiate / or explore alternative designs as
insurance keeping in mind the risks.
iv)
The engineering penalty of
supersonic speeds not kept in mind at the time of specifying. The
only but excellent example is between the North American F 86 Sabre and the F
100 Super Sabre which used the same technology genre- axial flow engines, gun
armaments, electronics etc. The results are tabulated in Table 1 below
The
table highlights the penalties even a marginally supersonic aircraft
imposes.
Table 1
Sl.
No |
Parameter |
F
86F Sabre |
F
100A |
Ratio:
F100/F 86F |
1 |
Max.
Speed |
M
0.93@S.L |
M1@S.L.
/M1.4 at 10k mts. alt |
1.41 |
2 |
Disposable
Load / Thrust kg |
151 |
81.5 |
0.539 |
3 |
Disposable
Load/Aircraft Empty Weight Kg/kg |
0.844 |
0.6585 |
0.78 |
4 |
Internal
Fuel / Max. Thrust kg ./ kg |
0.46 |
0.34 |
0.74 |
5 |
Wing
Loading kg/ sq. Mts |
330 |
450 |
1.364 |
6 |
Target
Volume |
562 |
943 |
1.67 |
7 |
Aspect
Ratio |
4.8 |
3.92 |
1.22 |
8 |
Engine
Thrust kN |
27.69 |
71 |
2.54 |
9 |
Wing
section thickness % |
9.5 |
6.5 |
0.7 |
The table suggests that an alternate AMCA designed
as a Transonic (M 0.90-0.95 at S/L) Intruder platform will carry 3500 kg i.e. almost
double the AMCA weapons load in “stealth” mode and the same total weapons load 7000
weapons load but with 20% greater range for an empty weight of around 9800 kgs,
using a total engine thrust around 3x40 kN or less. It would have lower
acquisition and life cycle costs. It would be significantly smaller,
cheaper, more versatile with lower detection signatures and yet do at least as
well in combat as the “standard specification” AMCA aircraft. In transit to
target -because of its internal stowage of the Brahmos – it should be as fast
as the SU 30MKI.
Military specifications do not
come from logical scenarios. They often come from what is technological
possible and greed for earliest profits. The M 16 rifle is a case to the point.
At one time it was not possible to produce a reliable 5.56 mm automatic rifle-possibly
because the metallurgy and the tolerances were not up to the required mark. When these challenges wee overcome the
Americans rushed in the 5.56 mm rifle prematurely into Vietnam. It suffered a
fate much much worse than the much-derided INSAS 5.56. Many Americans died because
of their faulty rifles jammed in combat. Their bodies were found trying to
re-assemble their jammed weapons. Everyone knew that the 0.22/5.56 was not a
killer weapon. Even teenagers had to be cautioned that the 0.22 could
kill. Yet the 5.56 mm became the standard calibre of all armies.
We have technology deficiency
made worse by lack of political ownership. For us reasoned debate over
specifications will yield solutions.
To be continued…
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