Saturday 30 May 2015

Preparing for Armageddon - Criticality of Developing Indigeneous Weaponry

The rise of new economic powers gives rise to forces which can well be described as ‘Tectonic’. The usual means of resolving such forces since the Punic Wars is prolonged and bloody war. India is re-emerging as an independent economic powerhouse and must expect and prepare for an eventual confrontation, possibly even war, with China and ultimately the USA. The contours of such a conflict cannot be discussed here. Perhaps the paranoid may be forgiven the view that the various ongoing aggressions - the funding and sustaining by proxies of terrorist and insurgent activities, the sustained support for Pakistan by the US, the building of encircling bases by China, the covert acts of cartographic aggressions and even the printing of fake currency notes are all carefully planned opening moves of a campaign to reduce and weaken the Indian State before administering the coup de grace. Sage political leadership may find ways of resolution by peaceful means but the precedents of such leadership being available are not encouraging. Thus sic vis pacem parabellum must be the urgent policy. Of the three protagonists, India is the least prepared for such a showdown. In our past wars sustainability of the war effort was not a significant issue but will be so in this future conflict. In sustainability our weakness borders on the grievous. Seventy percent of India’s war-making equipment is imported. A few years of remorseless sanctions and this shiny hitech equipment will become dust covered junk. An indigenous and comprehensive war industry is worrisomely overdue. Technical “challenges” are the least of our problems; ‘Timeliness’ is. If we have to be ready in time we have to reorganise so that the undoubtedly adequate available resources are best organised for timeliness. Wars can be deterred by having sufficient numbers of adequate, but homegrown, equipment to execute sound doctrines.

Reorganising...ad infinitum

“Whenever things go wrong we tend to reorganise and there is no better method of creating an illusion of progress when in reality changing nothing”. Quoted two thousand years ago by the sage Tacitus, this illustrates the inherent difficulty in reorganising. The authority to reorganise lies with those very people who created the problem in the first place. The disastrous track record of weapons development by the state sector was caused by the almost criminal flouting of the simplest rules of management. These failures can be easily corrected if the political leadership wills it. Even if “half improvements” are made in all the areas where mistakes were made, there will be a sea change. The starting fault lay in isolated development without a detailed interweaving with broader strategy. That misstep resulted in chasing the butterflies of latest technology. Confusion was worse compounded by keeping everything within state control and out of reasonable public scrutiny. India has lost time dangerously. The saving grace is that the skilled work forces of today are larger, the design resources have improved and if we can completely shed in defence R&D the wasteful dogma of over protective state control we may, with a few path breaking corrections, surprise ourselves at the turnaround.

The Need for Honest Doctrines

It was a British General who stated rather ruefully “You haven’t fought unless you have fought the Germans”. The truth in the statement can be judged from the fact that the Wehrmacht quickly overwhelmed European armies and then fought the two world superpowers for four years – and almost won! Every country has its doctrines .What made the Germans formidable was the emphasis they paid on honestly developing doctrines and their ability to incorporate available technology into their theories. German equipment was not superior. In fact the German KPzW II and III tanks that ripped France open in 1940 were inferior to the French Somuas and the British Matildas. What set Guderian and Student apart was that instead of trying to justify a concept (which happens here often enough) they went about with clinical impartiality (one could say sterility) to allow the idea to grow. The outcome of such “Brahman” (there is no better word) detachment from the result actually resulted in brilliant tactics and meticulous plans with a cascade of consequential studies and action. The sweep through the Ardennes required the landing of gliders on Eban Emael. When DFS gliders landed the Fallschirmjaegers on to the top of that fortress, the hollow charge weapons required to punch through the roof of the cupolas had been anticipated and developed. Impregnable Eban Emael fell within a few hours to a small and lightly equipped force. This is the end result of a coherent policy of the development of doctrines matured in the full knowledge of the political leadership which gave inputs of political will and sanction from the start. Two fundamental points need to be underlined. The first was the German readiness to use suboptimal but internally available technology to incorporate into their war plans. They used the Junkers Ju-52 as tow planes for their gliders because that was what was available. They did not insist on getting a manufacturing license for the immeasurably superior C-47 Dakota to equip their airborne forces. Equally important, the German General Staff, despite all its Prussian snobbery was reasonably willing to allow non Hochgebornen and relative juniors, the proverbial ‘man on the spot’, to develop and expound doctrines which may have “frightened the horses” in another Army. Guderian and Student were half Colonels when they set out their theories of Panzer and Airborne troops. Generals should be more occupied talking to the political masters (as did General Manekshaw in 1971) sorting out permissions and sanctions to mess around with sweeping ideas. Let that be done by ‘the man on the spot’. The problem with the ‘thinking General’ is that there can never be critical analysis of the doctrines as, during service, he represents the highest perfection in human thinking. Think dispassionately and make do with what you can cobble together. The Wehrmacht, planning for the more difficult war of aggression, thought honestly and based that thinking on equipment that was ‘homegrown’ (indigenous in Indian speak). We have to adopt their ways of gardening.

Bringing the Dogs out of the Doghouse

In India the bureaucracy (‘iron frame’ or ‘iron control’?) has sustained a prolongedand by now irritatingly petty campaign –to keep the Military in the doghouse. Immediately after Independence there may have been some reason but an aspirant ‘Super India’ cannot afford this upmanship. A state funeral for Field Marshal Manekshaw, with all its pomp and circumstance, would have been a great demonstration of Super India. Instead it appears the bureaucracy got its knickers in a twist about the precedence between a Cabinet Secretary and a Field Marshal! Shame! The Military has to be restored as an equal partner because there will always remain the doubt that even a brigade of the most obstructive babus will not halt the Chinese or the Americans: only the Armed Forces will. The babu -Politician nexus must be neutered to bring the Armed Forces out of the Doghouse and make them a respected party to the entire process of decision making at the War Cabinet level. What is the result of ‘dog housing’ the Military? Compared to the Prussian ‘Big Picture Brahmanism’ what we have is a predilection for the incoherent leading on to the incomprehensible. It appears (even 60 years on, the bureaucracy needs to keep its secrets dark!) the decision not to use the Air Force in 1962 came more from the inputs of the IB rather than from the professionals of the IAF! That too after the shooting war had started. The INS Vikrant is a telling case to the point. Did we go in for a carrier because there was a perceived maritime threat that overrode the Army’s/IAF’s need to prepare for mountain warfare or did some British FO babu let an Indian babu know that the HMS Hercules was up for sale and could be had at a reasonable price? Having got the Vikrant we had to wait for the PNS Ghazi to blow up before we risked it in the Bay of Bengal for a mere 3% (one hundred and eighty nine) sorties against a defeated enemy. For much less the Navy could have got shore-based Il-28s or Canberra squadrons which could have been more versatile and ‘expendable’. The question to be asked in sanctioning an aircraft carrier is, would the Navy risk its prize pig in an actual war? The same question arises when the Army wants MBTs that can make surgical thrusts into Pakistan. Are our politicians steeled (no pun) to permit such a thrust? Will the Americans/Chinese allow it? Does the Army’s culture allow it? Losses in defence are accepted but very few Brigadiers (being decent middle class chaps) will proceed if he begins to take losses in an offensive. If the answers are no, then Liddel Hart’s concept is irrelevant. Settle for the Arjun, its reliable even if it is not the “latest and best”. This is not the place for details but the experience of tank warfare in the Gulf wars is as relevant to reality as the bombing of Guernica was to prove that the fast bomber could survive in the face of opposing interceptors! The fault is not with the Armed Forces. As long as the Armed Forces are kept ignorant, they will insure themselves by asking for equipment of the highest technical merit without its relevance to realities. Note that the Wehrmacht was always clear of the political aims well before the war. If the strategic scenario is not settled the rest of the details cannot follow. Why did the HF-24 have to achieve Mach 2? Why did we buy the AMX-13s if we basically used them as mobile pill boxes? Why did the IAF lack hardened shelters? Why were Canberras, Gnats and Mysteres still in natural (silver finish) in 1965? Why was the raid on Peshawar carried out using single 4000lb ‘Blockbusters’ which, as the name indicates, are used against dense strategic targets? A load of 8x250 lbs would have wiped out the entire PAF force of B-57s.

Reining in the Bureaucracy

Such lapses indicate that war planning was inefficient and neglected. Since the Military was being kept out of the developing “big picture” the essential time required to plan was never available. When the ‘Desert Rats’ (LRDG) went to war they had the technical expertise of ten years of desert operations taught to them by archeologists who had spent time investigating Carthagian ruins in North Africa. The details went down to how to store maps – “don’t fold them-keep them between sheets of plywood”. Success in war is critical on detail. Compare that with our para commando’s gallant efforts (or picnic, if one is uncharitable) with Jongas in the Western desert. It is fortunate for us that the Pakistanis were just as chaotic. The concept of dropping parachutists at Adampur, Pathankot and Halwara was brilliant but the Pakistani planning details were a Buster Keaton comedy. One hopes there is not a re-run by the US First Airborne. There is a need for “thinking” which needs “time”. To obtain the necessary time, the bureaucracy and the Military must talk as equals instead of one devising crafty protocols so that only the other is frisked at our airports. “Frisk the lot” one can hear the public say. The same attitude problem bedevils the formation of a General Staff; a bête noir for the bureaucracy who are the only gainers in the inevitable inter-services rivalries that the lack of such an institution fosters. A Combined Chiefs of Staff (CCS) makes for coordination and efficiency. The force multiplier effect of the CCS can be gauged by the fact that after the First World War, the defeated Germans were allowed an Army and a Navy but not a CCS. We can no longer deny ourselves this potent force multiplier.

Operations Research is the key

“I put so little milk in my tea”, said the Irishman, “that you could hardly call it tea”. Like Paddy’s’ tea, we are taught to think OR is not OR if it does not have lots of mathematics. Our professors substitute mathematics which they can teach (after a fashion) for real experience which they never got. In OR, mathematics comes at the last to quantify the problems which OR has defined. Since disconnected mathematics is boring and meaningless, the present pedagogy has succeeded in frightening and confusing people off meaningful OR. That is unfortunate because OR is an outstanding zero cost force multiplier. What should be the TBO of our engines given that many engines will be downed due to FOD well before the brochure figures? What should be the actual airframe life given our flying conditions and CAT “E”rates? What are the “g”s we normally pull in Su-30 sortie profiles? What is the average g-loc level of the Indian pilot? What will be the reduction of effort in having standardised aggregates? What is the real shooting range for tank guns given our varying terrain? What are the weapons our intruder aircraft must carry given the accuracy of the bombing equipment? Will it be more effective to have a salvo of low accuracy but much cheaper SAMs compared to the imported ‘single shot’ wonders? OR studies could minimise our technology needs and the work burden in weapons development. Even in daily operations the impact of OR, done by practical men, can reduce the workload of preparing for war. There may be thousands of ‘Kaizen’ applications which will help in reducing the ‘run rate’ required if we are going to be ready on time.

Standardisation: de-optimise

The Soviets thought nothing of fitting the same AGD horizon on all aircraft from the Yak-18 basic trainer to the Tu-20 intercontinental bomber, over a hundred times bigger. This standardisation extended across all systems and aggregates that went into combat equipment, be they gyros, generators, batteries, instruments, heat exchangers. Unthinkable de-optimisation for the West, the dividends were huge: availability, reduced prices and simplified logistics; in short, optimised war capability. The Soviets, unlike the West, even avoided having a sacrosanct materials grade for aviation. Used to GOST they would laugh to see mild steel for a bracket being called DTD S1 and being imported with a release note. Our Government functionaries will not initiate this vital rejig. Why bother? The pension is guaranteed. They have to be re-educated. India’s automotive industry, having adapted the AS 9100, has quality standards which are often equal to the aerospace standards being followed. The Private Sector and its various collective associations such as CII must give the lead to re-examine current automotive expertise vis-à-vis aerospace technologies of fifty years ago. Russian standardisation went further. The TsAGI (their NAL) would investigate aerodynamic layouts e.g. the uniquely Russian ‘tailed-delta’ layout and leading design bureaus would further tailor the data for widely diverse aircraft such as the MiG-21, the Myasischev Bounder intercontinental bomber and the Su-9 all weather interceptor. If resources were so organised India would be the envy of many aerospace nations because of the vast, diverse and deep pool of world class technologies in aerospace/automotive equipment we have access to and experience of. What needs to be done is to examine our range of products and select for standardisation those which are most indigenisable completely and quickly. Being proof against sanctions must be the deciding criteria. Standardise ruthlessly. Compared to the MiG-27’s R.29B the M53’s exterior is so elegant that you could wear it on a tiepin. But is a jet engine for wearing on a tiepin? They are all alike as peas in a pod functionally. What goes for jet engines and ventilating fans probably goes for Army howitzers also if one sees what is being meant. God bless the Army but there was nothing wrong with the Bofors 155mm howitzer selection! Mount the Bofors barrel and systems on an expendable aluminum carriage to get an ultra light howitzer. Howzzat?

Limit the Technology

What Tacitus observed for ‘War’ is true in India for ‘Technology’. The enthusiasm for technology seems to be the highest with those with the least experience of it. It is painful to see the Government run weapons development organisations take on jobs that many have patently no experience or attitude for. Any discussion on aero-engine development, for example, soon gets in to jargon like SC blades, flat rating and smokeless combustors. Such jargon and its usage betray a lack of the practical. These fascinating technologies are not essential. For example low TBO is not a core problem. It can greatly simplify the timely development of an acceptable engine. The IAF will kick and scream but it can be persuaded to accept an engine that gives only 300 hrs TBO provided it was utterly reliable within those 300 hours, was easy to change and spare parts were plentiful. The IAF quite rightly will not accept any engine if it is ‘unreliable’.

No Time for Invention - Learn to Copy! 

The Chinese have a tradition of making painstaking copies: sneered at by the West – the word ‘Chinese Copy’ having insinuations of brainless copying – the Chinese have an admirable capability of getting into detail, reputedly the very place where the devil resides. It is significant that when we got the Gorshkov, the Chinese bought very cheaply the hulk of the Varyag for copying. Copying does not result in second rate weapons. Real engineers – those who by definition can do for six pence what any fool can do for six shillings – copy all the time. The Soviet strategic bomber force was built up within four years by Tupolev who was astute and humble enough to copy the B-29 from examples which had force landed in the USSR. “Legend in his lifetime” status notwithstanding, he would have returned to prison had he failed! The Tu-4 with its remote controlled turrets was ready for service with the Dalnaiya Aviatsiya in the stipulated time with numbers and reliability and gave the Russians the deterrent force they needed. Our weapons developments have been done by Governmental Scientists, unfortunately, without the persuasion of possible imprisonment. Having no effective experience or capability, it appears that connections, politics and ‘organisational tribalism’ decided the selections, the project leaders ignored the world’s richest and most diverse source of advanced weapons technology. They seem to have betrayed their lack of engineering abilities by starting with clean sheet designs. The national disaster, it is nothing else, is repeatedly there to see. To note is that the experienced French consultants to ADA, for example, stuck to their known devil of the tailless delta/FBW which was not the wisest choice for India. In fact they did not even venture to go from a 3-digital plus one analog channel (as an engineering concept it had much to commend it) to the ‘latest and best’ all four digital configuration. Apparently that added 4 years to the LCA’s delay. We have to copy and evolve for the present. For example we have a range of engines The AL-55(I), the Adour, the R.25, the RD. 33 and the AL.31F whose details we largely have. Let us select any three as our light, medium and large engines, with or without afterburner as singles and multiples cover everything from light trainers to strategic long range missile carrier aircraft. These engines should be copied not necessarily within the Government Scientist biradari but at the ‘Indian Nation’ level i.e. including the private sector with completely equal and fair advance funding! Current ‘Apex’ (jargon for bottleneck) organisations, especially the failed ones, must be turned on their sides to become ‘bus bars’ feeding detail technology to the teams. True, certain items such as rolling bearings and alloy elements and microchips need to be stockpiled but that is manageable. Of course the results would be suboptimal, in the way a Chinese J-10 or a Hong 6 is suboptimal but the US will think carefully before trying to take on China. Skilled designers can produce effective and affordable warplanes from the menu of engines and accessories that we already possess.

Innovation or ‘Jugard’

The other ace is to innovate. When Britain needed a multirole fighter to face the Germans, Frank Barnwell of Bristol, being an engineer, did not go about designing the ideal aircraft. He took the wings and tail of the existing Blenheim light bomber, married it to a slimmer fuselage and produced in time the Bristol Beaufighter, an aircraft that later revolutionised anti shipping strikes. The Soviets had a long tradition of adapting Naval guns for tank gunnery. At usual firing ranges they were effective. The famous 88, dreaded as a tank/anti-tank weapon, started life as an anti-aircraft gun. And so on. In the neglected area of AAA, the greatest harvester of enemy aircraft even today, our main need is not static but air transportable AAA. It may be wiser to use the gun and fire control of the Shilka, Tangushka or naval 76mm dual purpose guns as the basis of a range of static AAA weapons rather than design a new gun from the carriage up. Similarly barrage balloons on the approaches could reduce the efficacy of runway busting bombs. The possibilities are endless, given our resourcefulness.

Equipment for that War

Indian defence tasks for future conflicts can perhaps be summarised in the following:

» Denial of immune approaches to the Indian Coast by large Aircraft Carriers.
» Ability to thwart hostile advances in the mountains.
» Denial of using Pakistan territory as a spring board for launching military offensive operations.

The above abilities must be maintained in the face of prolonged sanctions over the issue of Nuclear Proliferation, carbon emission or similar pretexts. The roots of the Pacific War were in America imposing sanctions on petroleum and rubber to Japan for the same contemporary ‘outrage’ which was overlooked in the case of Italy. To stand up to such blackmail we will need totally indigenous weapons and vast numbers of them. The fright about the weaponry displayed in the Chinese Golden Jubilee parade was not advanced technology. The fright was that it was available in such large numbers and that it was all Chinese down to the last ‘O’ ring. Should nuclear weaponry have lower priority over building up sustainable conventional forces? During the 1960s, when China’s nuclear teeth were still ‘milk’, they routinely shot down any US aircraft that intruded into Chinese airspace because of Chinese confidence that any war could be sustained indefinitely. They knew their ‘obsolete’ technology was not ‘ineffective’ in the minds of the Pentagon. To put the mindless harping of ‘Fifth generation technology’ in the correct perspective, the reality is this: even as we talk of the FGFA, MCA etc, the IAF Chief of Air Staff, would be deeply grateful if he were given three hundred new build MiG-21s. If on the top of that, the fighter “landed slowly and did not burn up” he would feel a man reprieved. With this perspective in mind, the country needs to develop a range of simple, secure and effective warplanes.

The Simplest Air Superiority Fighter

Thus, the LCA nettle must be grasped firmly. As of present it is a ‘failure’. The LCA is not going to be ready in any useful time. No one loses his pension/ Padma Shri in case the 2010 dateline fails (yet again). Effective squadron service is like “Dilli, dur ast”. Technologically it is totally insecure. Even its material of construction is sanctions prone. The Su-30 suffers similarly with the added problem that it violates a cardinal rule of combat equipment; it is too huge. It will be, like the Su-7, vulnerable to low cost defences. The LCA will be an option once it is redesigned to be ‘sanctions proof’. The so called LCA Mk.2 must be recognised for what it actually is - an effort to undo the worst sins of the Mk.1. The detail engineering of the airframe was careless. To this end the airframe should be redesigned in aluminum and the detail design gone over with a fine comb by engineers rather than ‘scientists’. Working with familiar material, the stress men will achieve a significant weight reduction. The scope is certainly there. Once the weight is reduced, effective performance can be achieved with a copied R25/RD33. No engine is good enough to overcome careless detail design. Without a ‘sterile’ re-organisation, the LCA/F414 will be a re-run. The ideal (LCA) would have been a Gnat enlarged sufficiently to pack the MiG-21 Bison’s systems and weaponry in a new airframe which would conform closely to the Gnat’s aerodynamics and structural philosophy. The power plant would be again a ‘secured’ R.25 or RD.33 but without the afterburner as supersonic performance is known to be of little use and the Gnat concept is fine tuned for excellent transonic or ‘real’ combat conditions. The obvious improvements (LEX, LE Flaps etc) can come progressively in the Mk.X! ‘Scientists’ may not know enough to believe in scaling up (one actually spouted Reynolds Numbers–wrongly–to frighten the ‘ignorant’) but engineers know that the list of aircraft, including world famous ones, developed by direct ‘enlargement’ is as long as one’s arm! A scaled down MiG-29 using either AL.55s or non-reheated RD.33s and optimised for clear weather air superiority at transonic speed i.e. tuned for the regime where 95% of the combat takes place would be an option. You will still win the war because almost all the time you will be in the right aircraft at the right place at the right time and in the right numbers. If three simultaneous fighter projects seem much too much, remember that faced with a similar crisis, the Soviets sponsored twenty six! That was good management wisdom because they got three ready in time. Two of the three winning designs then actually saved Russia.

The Simplest Strike Aircraft

Two warplanes are envisaged in this category. The first is a minimum engineering revival of the Ajeet airframe to take the Saturn AL 55 engine, possibly with afterburner in the later models. Critics will say that the warload is too small. The improvement in AAA is such that the ‘Western cold war’ concept of a very large war load is now illogical. In actual combat the small size of the Gnat meant that not one was lost to AAA in the East though it flew as many strike sorties as the Hunter and the MiG-21 - the bangs per kilo buck were thus quite comparable. The turbofan and re-engineering will double the radius of action and far more. The second is a revival of the HF-24’s proven airframe to carry the MiG-21 Bison/Jaguar systems and equipment and powered again by the AL-55. It should be possible to provide additional over wing pylons like the Jaguar as well as a centre line pylon but many other ideas like LEX, or shortening the fuselage, can wait for the later marks. One important ‘human’ advantage of using proven airframes and systems is that not only can the work be reliably completed within three-four years but also the babus are less hesitant about certifying the bird! For the potential achieved by re-engineering a warplane of this class, read Vayu Aerospace Review II/1990 by this same Author. Past failures were entirely avoidable. The earlier Ajeet and the HF-24 Mk.1R failed because the ‘improvements’ pushed up weight and therefore drag but the engine remained the Orpheus. In the case of the HF-24 Mk.1R, the locally developed afterburner was so simple that it possibly even lacked a variable area nozzle. In fact these projects should not have even been tried! To add insult to injury the detail engineering, which really makes or breaks an aeroplane, was always a weak point with the organisations concerned. Recently it appears that an ‘expert’ from Germany had come and pointed out that the cable guards were fouling with the control runs in the NAL Saras. If true this is appalling but gives hope for the future! One does not need experts from Germany to point out such simple things- one needs Engineers who will get off their b***sides and crawl over the prototype when it is undergoing assembly. A mention of this is made to show that things are going wrong because the simplest rules of product development are being ignored.

The “expendable” Transports

Logistics form the backbone of warfaring capability. Without airlift capability some of those ultra light howitzers may end up in the Beijing and Washington war museums. Transports are needed and in large numbers. A enlarged version of the Otter or the An-2 and a revival of the Dakota or may be the Dornier 228 but with about twice the power will be needed. The same goes for a new avatar of the C-119 Packet but with turboprops or the An-12. Robert Watson Watts of HM Post Office, charged with getting the British Radar Interception system ready in time to meet the Luftwaffe, used to say something which is worth repeating because it is so relevant to us: “Don’t go for state-of the art. Cobble together the third best! The second best will be almost too late and the best will never come.”In fact the British CH and CH low radars were technically inferior to the contemporary German Freya, See Tackt and Wurzburg systems but it was adequate for the task and was available in right numbers in time and reliability to help win the Battle of Britain.

The High Altitude Close Support Aircraft

No Air Force likes to do close support work because it is not ‘their’ work; this disinclination makes them ill prepared for it and thus losses are higher in this already hazardous job. The mindless use of helicopters is an American concept. It may be good for Bell Textron but the Vietnamese guerrillas are still laughing about it. Helicopters are noisy deathtraps in an AAA environment and with limited high altitude capabilities. The conventional attack aircraft is too unwieldy. What is needed is an aircraft where the armament is turreted so that the aircraft manoeuvre envelope demands are not restricting the ability of bringing the guns to bear. The starting point could be most of the MiG-25’s fuselage and systems married to two HBPR turbo/prop fans and possibly a biplane configuration which has excellent handling qualities at altitude whilst remaining compact in size. Given the excellent record of the Il-28’s tail turret to keep Mujahedeen Stinger operators heads down during the withdrawal part of the firing pass, a tail turret (copy the IK 5!) would be a ‘must’ feature.

The Brahmos / Super Brahmos Carrier 

The Brahmos missile has great promise and we should work for enlarging it to a size that will give a range of around 700 kilometres i.e. enough to dissuade any hostile aircraft carrier to approach within effective launch distance of the Indian coast. Such missiles will need carrier aircraft. The most reliable route to development will be to scale up the Canberra-type by about 30% which will give a bomb bay of three meters in diameter and ten meters in length i.e. sufficient to carry three to four Super Brahmos together with the personnel and systems to acquire and operate the missiles. The power plant would be the unreheated AL-31 and all systems would be from the existing standardised aggregates. Such an aircraft would be cheaper, carry more missiles ensuring higher Pk, have better acquisition and control systems than the Su-30MkI, and yet be just as fast as carrying a Brahmos externally. In 1962 we lost a winnable war. It affected our lives more than one may concede. For a re-emergent India, confrontation with China and/or USA is inevitable. The US, in war, is wily, powerful and (against the Asiatic), ruthless. We lost in 1962 because of bottlenecks not in our resources but in our leadership, our ‘professionalism’, our planning and thinking and in our inability at the top to respect each other’s sentiments. The same situation exists today. It is at the top, perhaps less than a hundred people, who will have to re-orient their attitudes and co-operate. The rest will immediately follow. Given that we will not only acquire the wherewithal to defend our sovereignty but also project our unique brand of ‘soft skills’ for a better world. Time, however, is running out.

Friday 3 April 2015

The AMCA – Look before you leap!


The cost of the LCA programme  not including the engine is given as the arithmetic sum of all the sums released from time to time; it is somewhere around Rs. 8425 crores  E&OE. The present day value PDV i.e.adjusted for inflation would be closer to Rs.40,000 crores.  This is a four fold increase over the initial estimate adjusted to PDV. The time scale overshoot is of the same order. The money does not matter. It can be regenerated but the time lost is irreplaceable. That is the price paid for what is  the longest running development programme ever in aviation history. 
We are about to sanction to the same techno-structure the development  of a fifth generation aircraft the AMCA.  It is important to pause and think out the simplest of questions lest we get swept away by ill planned dreams. The AMCA is several orders of magnitude more sophisticated than its “4rh generation” predecessor. The time is now to passionlessly rethink. Significant changes in the techno- structure is indicated if we are not to repeat the LCA fiasco.

As a start we need to ask ourselves the following questions:

1. What is the Fifth generation and what is its logic?
2. Do we, India, need the so called Fifth generation?
3. Do we have the required base infrastructure to develop the fifth generation?
4. What is the level of usable research done to solve the detail problems posed by the new technologies?
5. What is a realistic time scale and a budget?

If we sweep aside these questions in our rush to “get “ the project or we trammel our thinking to create a “same as” product we may be squandering resources which could have been deployed elsewhere in the field of Defence Engineering. 

The Fourth and the Fifth Generation Reviewed

The so called Fourth generation introduced the following technologies into combat aircraft.

1. Composite structures
2. Fly by wire controls
3. Glass cockpit
4. BVR missiles

I will emphasize that the first three technologies were spurred by the availability of technology that was developed specifically for Civil airliners. In fact it would be impossible today to design an economically competitive main line civil transport without using the above technologies. For combat aircraft that imperative is doubtful. For Combat aircraft these technologies are useful if you have it “off the shelf” but not essential to give the other side a bad fright in a fight. The 4th generation is no more than a convenient index of the equipment sophistication level of the aircraft and it would be unwise to believe that a 4th generation will naturally beat a 3rd generation fighter. The best example is perhaps the MiG 29 initial production which had none of the first three (if you overlook a 8% use of composites for the engine nacelles- that too later converted to metal because of problems!) but it was THE bully on the block as far as air to air was concerned. On a lighter note if Airbus were to equip the A350 with BVRs legally it would be a 4th generation combat aircraft. Let us repeat the so called “generation” is a description of the technology level of the aircraft and is not repeat NOT to be automatically equated as an index of lethality in combat.

The Genesis of the Generations

The Fifth generation introduced along with the above technologies the following capabilities:

i) Supercruise
ii) Stealth
iii )Sensor fusion

The relatively poor performance of US equipment vis a vis the “crude” Soviet equipment in the Viet Nam and the Arab Israeli wars had a profound effect on US Military equipment design. The appalling losses suffered by the very seasoned Israeli.AF to Soviet SAMs in the Ramadan War led to a search for RCS reduction. From that direction Full stealth was then a small Yankee step. The back breaking logistics of Vietnam effort led to super cruise and the problem of controlling massed fighter strikes in clinically restricted airspace over hostile Vietnam territory led to sensor fusion as AWACS were horribly vulnerable where it was most needed. Sensor fusion was a form of phased array multiple dispersed AWACS! Both coalesced to form the Fifth Generation which is essentially a US oriented scenario requirement.

For example, the specifications that led to the F 22 Raptor required the following capabilities

i) Super Cruise
ii) Combat radius of 700 n.m.
iii )Stealth
iv) Cruise altitude of 21,000 mts.
v) Ability to operate from 600mts strips
vi) Sensor Fusion

Actually this bundle of requirements has less to do with direct general combat lethality and more to do with the American views of Power projection worldwide consequently Air Superiority over hostile territory. (Italics mine) which is fundamentally different in its level of technical sophistication requirements from air superiority over own territory.

Let us examine super cruise. USAF F 105s going to Vietnam would stage through from Mc Cellan AFB Sacremento California to Hickham AFB in Hawaii to Anderson AFB in Guam and then on to Takhli Thailand. It took three days, seventeen flying hours and 18 FR “tankings”. Considering the logistics problems a cruise altitude of 21,000 mts. was mandated to reduce the number of “tankings” because of the air density and hence drag would come down by one-twentieth of sea level. The high service ceiling was also required to achieve that “long reach” combat radius of 700n.m. A combat radius of 700n.m., you will note would cover most countries of the world bar three or four. The cruising altitude led to full stealth requirement as the aircraft would be easily “visible”. It worked both ways; At 23,000 feet the radar returns were sixteen times less than at 11,500 mts. Super cruise was introduced to cut down the transit time. TVC was needed because at 23,000mts the reduced “q” values made conventional aerodynamic controls sluggish. The other requirements such as AESA and sensor fusion consequentially became necessary because the aircraft being deep over hostile territory would lack AWACS support/ADGES support. This immediacy of information updates urges the need for AESA whereas a defensive fighter would be updated from ground based systems. Whilst AESA is fine if you already make it, it would not be quite such an imperative as it would be for the US strategy. Note a defensive aircraft would get from ground based support system all the information updates almost instantly and that too as a”voice over the shoulder” i.e. reducing the pilot’s workload and that too without any increase of the empty weight of the aircraft.

The American aircraft achieved enviable operational autonomy but at technical and fiscal costs that are unattainable for most nations. In fact for countries not having global aspirations the American specifications are unattainable folly because each Raptor costs reportedly $ 900,000 million if one factors in the development costs and the operating costs of around $68,000 per hour. These values presumably do not include the enormous global infrastructure- bases, tankers, hangars for stealth storage etc that only the USAF can have or afford. I will stress that many of these 5th generation capabilities are more useful for “spotting” the aircraft at distant bases than actual combat lethality. One of the many penalties of stealth is that the war load is ridiculously low.  If the past is anything to go by the Raptor and the F 35 may well prove to be poor in terms of cost effectiveness when opposed by the generic LCA operating within ADGES.

Most “sacred” specifications have an element of what used to be known as “bull dust baffles brains” in them. Let me raise a “Molesworth, the horrible schoolboy” question! Please, sir! Supercruise cuts the transit time by half. However the FR tankers barely do 400kts. The 5th generation aircraft will require refuelling every 70-80 minutes or so. What will be the effect of the frequent hook ups on super cruise gains, Sir!? To remember is that super cruise will need the most advanced technology of engines available only to the West.

We do not appear to have the base yet to manage a “predictable” AMCA programme. For India we must examine the thought that the counter to a haunting ghost is not your own ghost but the Ojha (witch doctor)! The counter to the Raptor may well be not another Raptor but the improved methods of stealth stripping, methods of confusing or degrading PGMs accuracies and destruction of aircraft at high altitudes using thrust vectored  missiles and new warheads effective at ultra-high altitudes where the blast effect is almost nil.

The scenario is everything- the “generation” less so!

The generic Light Combat Aircraft (gLCA) is a “defensive” fighter designed to an austere philosophy that less is better. It cannot be compared to an F22 point for point as one may compare cars in a catalogue but in actual combat it has been historically proved that the LCA will always outperform the “full service” fighter. There is no magic involved. The LCA uses “offboard” facilities- ADGES , SAMs etc to supplement what it is carrying on board. Let us consider the following scenarios:

1. When FO Nirmaljit Singh Sekhon took off on his intercept mission against six Sabres his chances was about the same as Leutenant Werner Voss’s epic fight i.e. about 3%. Would his chances of survival improved significantly if he had been flying a F22 Raptor? This assuming, of course, that a F22 Raptor could be scrambled within 40 seconds like yon Gnat of yore! Moving forward into time if his hypothetical Raptor was facing even the F6 or the F7Ps would he have survived? I do know that if FO Sekhon had a wingman in place his chances would have improved by a factor of ten!

2. The chance of a Bison surviving against an F 22 with both aircraft heading towards each other at 20,000 mts 90 km apart at M0.9 is in the low 20 per cent. What is the probability such a situation will occur?

3. What would the “game changing” role Ground based systems of stealth stripping, particularly; IR scans play in warning the Bison which would be over “friendly” territory? So what will be the number of MiG 21s which will be “helplessly” shot down by the Raptor? If the Raptor can be detected by IR “Radars” can it be brought down or its efficiency “laughed to scorn” by SAMs modified for High altitude intercepts?

4. Comparing the specifications of equipment and performance of the third generation Mirage III, the F 105 and the F4s against the 2nd generation MiG17  apparently the MiG 17 is a no hoper. In the wars over Vietnam and Arabs the little MiG 17 achieved remarkable success in Air Defence and Ground attack even when flown by crews whilst lacking nothing in courage, had standards of training which were no match for the Israelis and the USAF & USN high standards? In fact it was the US that went back to school and the highly professional Israelis never repeated the Aswan clashes.

5. Relevance of the equipment is everything. Possibly because of the quite effective PAF B57 attacks in 1965 the IAF chose the ‘better” MiG 21FL with a bigger radar over the MiG 21F-13. Analysis of the sorties as given for example in “Eagles over Bangladesh” would show that the selection of the MiG 21 F 13 for the first squadrons may actually have resulted in the PAF having several Sabres less. Could it be said that the R2L radar was more  of a nuisance than a help? You would have noted however that the Radio altimeter was much used to maintain height hold in the LLXCs flown.

6. I feel that we do tend to get carried away by foreign requirements completely irrelevant to us. There has been appearing on the Net (where else?) a rather well informed -be it said- discussion on “hot refuelling” as a means of reducing turnaround times. My own reactions are:

i) “hot” refuelling will not reduce turnaround time because in India brake cooling can be the problem. As an aside the LCA reported brake cooling problem will go way when the weight is corrected.

ii) Hot refuelling is extremely hazardous with plenty of chances of accidents.

The Swedish AF has hot refuelling because if you shut down a fighter in the Tundra getting it started again –in the open- may be a devil of a job. The German F 104 crashes were partly due to an idiotic decision about “getting the fighters used to the German weather”! The point I always stress is that we will be cheated if we use without due circumspection the thought of others. Is the AMCA something like this? A peasant’s scepticism for the new-fangled/ over advertised is not a bad quality for a designer!

There has been a constant marketing effort that somehow the 5th generation is somehow the ultimate weapon for dominating the skies but in reality it is a highly specific weapon- you will note that the US closed the Raptor production after only 187 aircraft. Either they have a lemon on their hands and are too proud to say it or it is so specific that it is sine qua non for certain USAF scenarios and- dare I say it - completely stupid for others.  We must think of our scenarios. China may need the F 31 in case they plan to takeover Quemoy or Formosa sometime in the future. Do we want to take back Askai Chin and will the AMCA help in such a scenario and does the cost indicated includes the cost of the associated infrastructure?

Whistling in the dark-  a review of the present 5th generation aircraft.

Reliable information on the 5th generation is hard to come by so cum grano salis here is my take on the current crop. The F22 is the gold plated thing. It really is a marvel of technology and American skills in manufacturing expertise. It incorporates all that the US learnt in ferrying its aircraft all over the world and in the use of the F117 in Iraq and from the B2.

The F22 is the gold plated thing. It really is a marvel of technology and American skills in manufacturing expertise. It incorporates all that the US learnt in ferrying its aircraft all over the world and in the use of the F117 in Iraq and from the B2. 

1. Sanctioned August 1985
2. First flight   September 1990
3. First Production aircraft 1997
4. End of production with 195 aircraft in March 2012.

They took 12 years to get the aircraft to IOC in spite of considerable experience in developing and operating with previous two service aircraft the F117 and the B2. Note that they took 27 years to design build test produce and write  finis to the programme. 

The Russian PAKFA is a very sensible middle of the pack design typically drawing on the Sukhoi/ MiG layouts and just “stealthfying” it much as our Navy has done to its frigates. It would be a surprise if a lot of its under skin stuffing was not from the Sukhoi 30. It is the most “right looking” of the crop which I cannot say about the formidable Raptor which looks like a jet age Jug (Republic P47 Thunderbolt)

The Chinese J 20 is probably a dark horse. It is of a Chinese concept of “Sashoujian”- the Assasin’s mace”.  It is larger than the F22 (23 mts. against 18.92 mts for the Raptor) and has less powerful engines but it uses an interesting “long coupled” canard delta configuration. The configuration will give a good CG range hence the ability to handle a greater variety of weapons. My guess is that the Chinese may be thinking something like this- if stealth is so good I don’t need to go fast. Better I use the power to increase the size of my weapons bay and carry a decent war load so that over Quemoy or Taipei I can loiter around and hit multiple targets using “invisibility” i.e. the Chinese aircraft is a technology demonstrator/ stealth Intruder/bomber and is not ,sensibly, a fighter to match the F22. The Chinese J 21 is inspired by the Raptor but somehow is a daintier looking design.

The Indian AMCA

There has been two AMCA mock ups and frankly it continues to show the lack of design supervision of details  that ADA is becoming well known for!. The first issue was the fin. It looked as if it had come off the HAL HA 31 Basant Ag aircraft!. This near vertical leading edge is un stealthy and certainly would have led to controllability/ structural problems at high speeds. This has just recently been corrected and we have a stealthier fin on show. The other is the intake! Sure the Raptor has splitter plate intakes – which are unhappy stealth wise – but the Raptor was conceived 30 years ago. I had hoped to see diverter less supersonic intakes (DSI). Is no one in ADA looking at the JF 17, the F 35 or the J 20? There is also the question of how the design does not seem to have taken too much care to “mask” the A/B petals by the empennage- the F35 and J31  does make the effort. Finally the information on the net about the AMCA is ludicrous in real terms. The thing is supposed to be capable of carrying the Helina ATGM! Why should anyone even think of wasting a rare resource like the AMCA on close support duties! Really! About the AMCA being capable of carrying Brahmos (stealthily or otherwise) strains the imagination. How does one carry a Ø 650 by 6558mm missile between the nose wheel well and the front engine face of a 16.570 airframe is doubtful even if the air launched version needs a shorter booster. The relatively low operating ceiling means that the radar returns will be 3-8 times larger.  These may seem trifles but as the ancient said so tiresomely long ago- hae nugae in seria ducent mala- “These trifles continued will lead to grave evils”.

Do we need the Fifth generation?

The 5th generation programme is a political statement that we are ready to play Bully Boy in the neighbourhood.. Whether we invest people and effort on a colossal project like the AMCA will have to be decided by the people who will decide the country’s foreign policy. The PMO, MEA, MoD and MoF with inputs from the Armed Forces. It has to be a very careful assessment of the threats, their likely time scales with the Armed Forces going deeper into the targets- bridges, dams, air craft carriers, installations, the weapons likely to be sanctioned for use and the tactics to be followed and the infrastructure to be put in place- training, people, tankers, bases and hangars et al i.e. a total system has to be estimated before the development agencies are brought in to the picture. We know what happened when the customer was side tracked to fast track the earlier project.

What will it cost in time and money? 

The earlier LCA cost us Rs. 40,000 Crores so far. This was mainly due to sheer mismanagement and it would be “optimism” to assume that we have learnt from the earlier project. We have learnt technical skills which we always had but there is no evidence, given the uncertainty about dates, of improved management. A budget for the AMCA should be around Rs 100,000 crore not counting the engine. The Fifth generation being a political statement as much as it is a weapon it makes little sense politically if we do not develop the engine. So we are looking at something in the order of 150,000 crores. The time for development can be approximated by noting that the Americans times for the F22. I would doubt any target figure short of twenty years ie. 2035 before IOC as a “salesman’s optimism”.  What will be the political compulsions and priorities by then?

What is to be done

The Kaveri failed because the basic facilities required for doing the projects were not at hand. As in the LCA the problems were compounded by not separating the problems into details before- integrating them in the package. What the design agency must do is to identify the problems associated with the development of the 5th generation and solve them in detail. There could be as many as 500 such problems but I am listing some of the more obvious ones.

1. Unlike ordinary “supersonics”, a super cruiser will ‘soak”. Its skin will soak at 125 °C whilst the core structure may be at - 65° C. How does one attach a composite skin to metal structure both having widely different co efficient of expansions reliably so that in service stealth, is not affected. I am emphasizing this because the LCA is supersonic for a few minutes at best and will not “soak” as the AMCA skin will.

2. Because of the high skin temperatures of 125⁰ C stealthiness is compromised to IR scans. The trick is to cool these areas using coolants or fuel. What is the standard of preparation on this as far as laboratory work is concerned? Same with cooling of the jet efflux.

3. Stealth requires Radar anechoic chamber to confirm and refine the shape being chosen w.r.t. radar returns? Have we already got such chambers? And what is the skill we have developed so far in validating the experiment with theoretical studies?

4. Stealth requires careful detail work. Gold flashing the canopy, minimizing the radar returns from joints such as panels and door etc. How much work has been done so far?

5. “Simple things” like drain holes caused problems between “stealth” and “corrosion damage” on the Raptor. As I said these are typical of the many questions that have to be asked and solved before taking up the AMCA  The standard of preparations regarding the sub problems are to be examined by a body independent of direct and indirect influence of the controllers of the programme funds. From past experience the usual panel of “eminent scientists and professors” would be the worst choice. What is needed is “engineering” common sense and experience.  There is also a somewhat naïve belief that CAE will can usually replace an experimental approach. This is partially true but with the tricky caveat that CAE is most useful to those who need it the least i.e. the seasoned engineer! CAE is very useful if one has identified and quantified the problem. It then allows rapid “optimization” Unfortunately the computer is politely silent if the engineer does not focus on the problem! This is more common than one supposes. Just one example from “open source”: In the HF 24 the ballast weight was – in the days of slide rules- 134 kgs. In the LCA, where with CAE one can get the CG at the push of a button- the ballast should have been ideally less than 50 kgs. If what is rumoured- 300 kgs- is true- it illustrates what I have said. The other and I speak from my own years in a large e- engineering firm is that rare is the engineer who will look at a screen and say with confidence “Yes! That is right! We need to do such and such!” Thus my caution about computer enthusiasm.



Divide et Impero!

To go bald headed in to the AMCA would be to repeat the LCA experience- the unfailing folly of introducing unproven technologies on an unproven platform. We should rather break up the job into technology modules:

i) Stealth technology
ii) Sensor fusion technology
iii) Supercruise

Stealth technology and sensor fusion technology has priority. Super cruise needs the most advanced engine technology and firstly it is not available at a corporate level or else the enterprising Chinese would have had it by now. They are beavering away at their WS 13 Taihang engine. We should better drop the engine for the present or we will be spreading too thin. The Kaveri programme showed we lacked the basics when people rushed in with enthusiastic promises!

Stealth technology has the following features.


i) Hard chine (as in small boats) fuselages
ii) RAM
iii) Intake masking
iv) DSI
v) Internal weapons bay
vi) Serrated panels and covers
vii) Gold flashing of the canopy etc
viii) Stealthy gun ports, AESA/SLAR installation and IR scanners
ix) Design, production and maintenance of pressure cabins with angular exteriors.

Since the AF is not exactly prancing with joy about the Mk.1 it would be possible to convert the last six airframes to a LCA Stealth model incorporating the stealth features. These six can be built to an “experimental” rather than a “combat” standard. For example the internal weapons bay need not be capable of handling all the weapons planned for use or the stress levels need not go to 9 g etc. The idea is to give everyone –designers, planners, operators  much needed “hands on” stealth experience. Because the aircraft is based on a “proven” design a first flight by early 2018 and completion of field testing by early 2020 is expected particularly given the confident enthusiasm being proclaimed for the AMCA project.

These aircraft will explore the following:

i) Stealth effectiveness
ii) Stealth maintainability, particularly in humid and dusty conditions
iii) Manufacturing and airframe ageing effects on stealth deterioration.
iv) Problems of stealth in LLXC profiles.

Since only three countries are in stealth technology it would be arrogant to presume we “know stealth”. We know nutt’in yet! The accompanying sketch shows a possible adaptation of the LCA Mk1 to a LCA Stealth Research Vehicle. The effort will be to confine the changes to the fuselage and see how some of the problems mentioned above show up in actual conditions. Similarly should be the approach to developing Sensor fusion. Sensor fusion has applicability even in ordinary strike sorties and so has priority over supercruise. The capability can be developed using a flight of Embraer145s or Dornier228s. These are roomy aircraft and will allow much space for a “bread board” approach and will confirm the technology and its bugs before final packaging. CABS and team would be an obvious resource given the work they have turned in on the Embraer AWACS. The obvious advantages of using a proven platform is that the testing is not held up whilst the platform itself is getting rid of its sinuses as happened with the LCA.

A Stealthy Foxbat?

Assuming that we still feel that a 5th gen “super cruiser” is essential it would be much wiser to have a very careful “engineer’s” look at the MiG 25 Foxbat and develop our own stealth aircraft based on the excellent proven high speed aerodynamics, systems and structure of the aircraft and “stealthifying” it rather than go off the deep end with a completely new and must I say it- sloppily configured aircraft.  Incidentally the MiG 25 would handle a Brahmos internally! 

It would be possible to go on but summarizing:

1. The 5th generation is a political weapon. It gives an aggressive message that we want to play the bully of the block.  Is that our priority?
2. It is a doubtful asset and requirements are too small to be economical.
3. The possession of such aircraft by our future adversaries cannot be countered by our possessing similar weapons. From these follow:
4. Our priority is not a 5th Generation but countering them e.g.

     i) Development of stealth stripping techniques
     ii) Development of techniques to confuse and degrade PGMs
     iii) Development of suitable SAMs
    iv) Development of structures capable of defeating bunker busters. Try Kanchan armour slabs for roofing?

If after this we still need a 5th generation we can go for a half house solution with emphasis on “range/payload capability” i.e. a carrier for the Brahmos as a priority rather than a “me too” Raptor like AMCA.

Surprising Even Ourselves

Finally we must return to the problem mentioned in the techno structure. Until this is energetically and drastically revised without the baggage of obsolete ideology we will waste and fail. To rephrase an Old Testament saying “But for the Government reviseth the structure/ the engineers will toil but in vain!” The socialist pattern of society of our infancy chose to believe that only the Government Departments and the Public sector was the worthy and trusty repository of public funds. The fact is as repeatedly demonstrated e.g. the Tatra truck affair that money has no respect for which side of the economic theory one is on. I give you the case that suppose the Government had selected say Tata’s or Mahindra or L&T for the LCA project and they had turned in the very same “results”. What would have happened? How would the Press and the Parliament react? Why should performance which could have been early declared as a swindle or scam be accepted with some nursery admonishment of better behaviour from the CAG if done by the PSUs or Government? Given the proven disappointment with the present arrangements, the present Government should grasp the nettle firmly:  Restructure drastically.

The Government must dismantle the “Commanding Heights of the Economy” mind-set so beloved of theoretical economists of a certain hue. Commanding heights gained by decree rather than excellent effort soon turns into Toll gates.
For weapons development all countries use the entire resources of the country. By keeping the private sector out or emasculated we are denying our weapons Industry the larger more vibrant and enterprising portion of our Industrial strength. Talk about going to war with one hand tied behind our back.

I have talked enterprise. Enterprise is the difference between Air India International a small airline under JRD Tata and the present day Air India. A Command economy cannot, by doctrine, have enterprise.

Welcome the private sector without bureaucratic caution. The Government must involve the Private sector as a valued resource rather than convicts on parole. Allow FDI without limits. Indian Industry is the only one in the world where the domestic automobile industry has successfully fought back the challenges of well-established international Giants. Why should they fail in the field of Defence? Those who raise the long dead ghost of the Honourable East India Company should be reminded of the “bogey” they had raised earlier:

1. Computerization will lead to loss of jobs.
2. Mobile phones will lead to loss of sovereignty (sic) and we should go in for the C DOT RAX- a 100 line rural automatic exchange.
3. Liberalizing the Automotive Industry will result in a foreign exchange crisis. 

Given this kind of accuracy of prediction the opposition to 100% FDI is short sighted or aimed at proving a certain economic theory rather than pro bono publico. Along with the  big giants will come also the small brilliant firms the likes of Burt Rutan of Scaled Composites and designers of the class of Stelio Frati and innovators like Edgley who would find that the canvas of India the ideal medium for their dreams. I have in mind also the Swiss ALR group who in the 1980s was working on the interesting Pirhana light Fighter. In India, with the same funds, they could have progressed five times as much. The FDI policy must be particularly tuned for such enterprises and encouraged at 100% FDI.

The present Government’s task is difficult because it must change the way people think! It must breakdown “the narrow domestic walls of our thinking” so that thoughts merge into broad urgent streams. If we do that we may surprise even ourselves.