araz
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A lot has been written on the subject of whether PAF should relook the issue of JH7s for its naval role. I think it needs a new thread for appropriate discussion.
I will request the Moderators to kindly shift he posts from M3/5 thread to this thread.
Here is the excerpt from Air force technology.
The JH-7 is powered by two Rolls-Royce Spey Mk202 turbofan engines. Each engine can produce 54.29kN of dry thrust and its thrust after burner is 91.26kN.
"The first JH-7 prototype was rolled out in August 1988."
The engine is 5.2m long. Its diameter is 1.09m. The dry weight of the engine is 1,856kg.
The Spey Mk202 engine was introduced in 1960. The engine was first received by China in 1975.
China signed an agreement with Rolls Royce in 1975 to reproduce the Spey Mk202 engine through reverse engineering.
The Chinese produced engine is designated as WS-9 Qinling turbofan engine and its trail production began in 1976. The WS-9 incorporated in the JH-7A aircraft is a licensed copy of the Spey Mk202 engine.
Performance
The aircraft can fly at a maximum speed of 1,808km/h. Its cruise speed is 903km/h. The normal and ferry ranges of the JH-7 are 1,759km and 3,700km respectively. The service ceiling of the aircraft is 16,000m. The aircraft weighs around 14,500kg while its maximum take-off weight is 28,475kg.
A
I will request the Moderators to kindly shift he posts from M3/5 thread to this thread.
Here is the excerpt from Air force technology.
The JH-7 is powered by two Rolls-Royce Spey Mk202 turbofan engines. Each engine can produce 54.29kN of dry thrust and its thrust after burner is 91.26kN.
"The first JH-7 prototype was rolled out in August 1988."
The engine is 5.2m long. Its diameter is 1.09m. The dry weight of the engine is 1,856kg.
The Spey Mk202 engine was introduced in 1960. The engine was first received by China in 1975.
China signed an agreement with Rolls Royce in 1975 to reproduce the Spey Mk202 engine through reverse engineering.
The Chinese produced engine is designated as WS-9 Qinling turbofan engine and its trail production began in 1976. The WS-9 incorporated in the JH-7A aircraft is a licensed copy of the Spey Mk202 engine.
Performance
The aircraft can fly at a maximum speed of 1,808km/h. Its cruise speed is 903km/h. The normal and ferry ranges of the JH-7 are 1,759km and 3,700km respectively. The service ceiling of the aircraft is 16,000m. The aircraft weighs around 14,500kg while its maximum take-off weight is 28,475kg.
The only problem is PAF seems blissfully unaware of this need and has not evaluated this platform since the late 80s. What was rejected in the 80s is unlikely to be accepted as the basic flaws in the design are not rectified and the engine remains pathetic. It seems that other forces world wide share the same view as to the best of my knowledge no one has expressed any interest in it barring Mr Mastan Khan and a few of his avid followers. If you look at the PAF philosophy it wants multirole platforms rather than single role ones. That maybe why it has not ben considered. With the J series running on WS series engines it maybe a better bet at the fighter bomber role than the JH7 provided China can work round the restrictions imposed on it by Russia regarding sales to third party.I think it's the side-discussion re: a potential Mirage III/5 replacement. As @MastanKhan brought up from the very start (here's ur credit man), the JH-7A is basically the only fighter-bomber solution available to the PAF in as far as lobbing big SOWs (H-2, H-4s, Ra'ad, Ra'ad II, and Mk. 84-based REKs) is concerned.
And, to be honest, he's right -- if doubling down on more JF-17s is the only route, then why not shore-up the heavyweight stuff using the JH-7A while using JF-17s as escorts/support fighters?
A
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