zebra7
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Dr. Tank, even while designing what he did for the Luftwaffe, did not have a specific engine in mind, so there goes your theory. You need to read up on the various combinations tried, until they settled on the happy final choice for the 190. The same thing happened with the Marut. Unfortunately, unlike his earlier experience, he did not now have the full attention of engine makers; in fact, they treated him with cavalier disdain.
Nowhere does one size fit all.
Ok here is my theory.
Experience with the license production of the Vampire and the Gnat led HAL to accept an IAF requirement of an advanced combat aircraft. Dr Kurt Tank (of Focke Wolfe fame) and his deputy Herr Mittlehuber were invited in Aug 56 to head the joint design team (Willy Messerschmidt having refused the offer and accepting the Spanish Government’s (later taken over by Egypt, Syria and Yemen (UAR)) offer to head the design of the Helwan fighter HA-003).
Originally planned to fly with the 3700 Kg afterburning Orpheus B.Or 12 (Bristol Orpheus) engine and let down by successive failures to acquire the RB-153, SNECMA Atar 09K-53. the super Atar M-53 and finally the RB-199, the HF-24 entered service and served for the rest of its 15 year career with the critically underpowered license built Orpheus 703.
The aircraft will be remembered for its superb handling being called the “Super Hunter” by its pilots. A promising design that could cruise supersonic at 40,000 feet, the Marut finally met a disappointing end thanks to un-kept promises and international politics that embroiled HAL and several successive engine vendors. Thus ended India’s first true fighter design.
source HAL HF-24 Marut - Where the wind blows
Here are the specs of the engine used in Marut -- uprated engine of GNAT -- Mk.703: Rated at 4,850 lbf (21.57 kN)
But Marut was desinged around Orpheus Bo.12 rated at 6,810 lbf (30.29 kN) dry and 8,170 lbf (36.34 kN) with afterburning.
So My theory as described by you, DR. Kurt Tank designed the Marut around Orpheus BO.12.
Nowhere does one size fit all.
Never did I claimed that, but many times the engine could be replaced with another one, and in that case the parameter to take care of is wt., thrust, air massflow and CG of the plane with that engine.
Dr. Tank, even while designing what he did for the Luftwaffe, did not have a specific engine in mind, so there goes your theory. You need to read up on the various combinations tried, until they settled on the happy final choice for the 190. The same thing happened with the Marut. Unfortunately, unlike his earlier experience, he did not now have the full attention of engine makers; in fact, they treated him with cavalier disdain.
No plane is designed without an engine. And the theory that after designing the plane without any specific engine, and afterward find the suitable engine is a flawed one, because the CG -- Center of Gravity have to be taken in consideration, and the wing design could only be made when you know, what is your thrust, and without knowing the Mass flow of the air though the air intake, the airintake nozzle could not be designed, and without knowing the wt. of the engine itself, how could the designer design the airframe.