This post is to share the experience and approach of China to development of its indigenous aircraft and aeronautical industry. It makes an interesting comparison to ours and has lessons for us to learn. The objective is to not run down any organization or armed force but to lay out the facts - the black, the white and the grey and let you, the reader, judge for yourself.
In the 1960s while we were trying to mature the Marut from a prototype to a fully developed squadron aircraft China had similarly started to manufacture a copy of the Soviet Mig-19. The Soviets shared the design in detail and initially provided some help but then the Sino-Soviet split of the late 1950s spilled out in the open and the Chinese had to go it alone with an attempt at re-engineering. They got the first copy off in 1958 and made a few dozen pre-production examples none of which met the quality control standards of the PLA Air Force (PLAAF) and this try-fail-retry continued till around 1965 when the Chinese Mig-19 equivalent the Shenyang J-6 (also called F-6) finally got into full service.
Shenyang J-6 air defense fighter, copy of the Mig-19; 4500 were built
While on paper the J-6 was a copy of the Mig-19 it was initially, at least, short on avionics and the engines, Wopen WP-6 (reverse engineered Tumansky RD-9), were qualitatively short on metallurgy much to the chagrin of the Air Force maintenance engineers. The aircraft had a MTBO (Mean Time Between Overhaul) of a mere 100 hours.
But the Chinese did not give up nor did their Air Force say forget it I'll buy abroad (in all fairness they didn’t have that option politically speaking in the 1960s or 1970s).
The Shenyang J-6 was built till 1981 and the later production batches had a significant improvement in metallurgy and finish. In fact their finish and production tolerances, according to the Americans, got better than the Russian built Mig-19. The later version also got their avionics suites albeit basic ones and were mated to early heat seeking missiles. In the 1970s when this aircraft was the mainstay of the PLAAF it faced the superior Mig-21's on the Indo-China border and Mig-21's and Mig-23's on the Sino-Soviet border. But they understood that large scale home production with no risk of spares being choked and standardization of training had its advantages.
Nanchag Q-5 ground attack development of the J-6; a close comparison with the HF-24 Marut
With their confidence building they re-designed the Shenyang J-6 into the ground attack Nanchang Q-5 (also known as the A-5). The PLAAF did not lay out specifications to match the Mirage III, McDonnell Douglas Phantom or the Mig-21 the hot fighters of the 1965-1970 period. They instead said lets improve on what we have and take it as far down the design road as we can. The air intakes were moved from the nose to the cheeks, making way for a planned radar in the nose, the fuel capacity was increased, more weapon pylons added and most importantly the air frame was stretched to accommodate an internal bomb bay of 4 metres. This stretch was done in a way to reduce drag at transonic (ie close to the speed of sound) speeds. This drag reduction enabled the Q-5 to fly as fast as the J-6 at sea level with the same engines even though it carried a much heavier weapon load. The Q-5 evolved into a basic but proven ground attack aircraft for close air support (mainly for army operations). But nothing is ever perfect. The Chinese were unable to develop a reliable ground attack radar, the PLAAF was not happy but still went ahead with a production run of ~ 1300 machines. The first entered service in 1970 and by the 1980s the radar matter was sorted out and even a anti-ship missile carrying version came in.
They kept it in production for exports till 2012, 54 years after their first attempt to reverse engineer the Mig-19. In comparison our Marut HF-24 had a slow production run of about 9 years and the opportunity to teach ourselves how to mature our own design and then improve on it lost. The J-6 and Q-5 more than any other aircraft laid the foundation of the Chinese military fighter industry and design capability.
This post is not about the details of the J-6 or the Q-5 but to illustrate what gets done when the user, designer-builder and the political bureaucracy work in unison to say it is our collective aim not only to get a reasonable (though not the latest or greatest) aircraft into the hands of our Air Force but equally it is our aim to develop indigenous design and manufacturing capability. This unity of thought & movement was lacking in the Marut story and I hope will be learnt for the Tejas journey hereon at least.
An interesting comparison of the Marut with the Q-5;
Top speed : Marut 1112 kmph at sea level; Q-5 1210 kmph at altitude
Attack radius lo-lo-lo : Marut 396 kms; Q-5 400 kms
Empty weight : Marut 6195 kgs; Q-5 6375 kgs
Max. Take Off Weight : Marut 10,925 kgs; Q-5 11,340 kgs
Weapon payload: Marut 1800 kgs; Q-5 2000 kgs
Engines (kgp) : Marut 2200 x 2; Q-5 3750 x 2
Production run: Marut 147; Q-5 1300+
The 3 aircraft were of the same genre and vintage. The Marut in fact had a superior wing design than the other two. The production runs tell the entire story of the two countries' approach to building indigenous capability.
We are the only country in the world which can send probes to the Moon and Mars, design & build Naval destroyers and aircraft carriers but cannot for the life of us get a jet fighter into service. Jai Hind.