Echo_419
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The Pratt & Whitney PW545B on board the General Atomics Avenger gives a thrust of 3991lbf or around 17.75kN.
Dimension wise the Pratt & Whitney PW545B is,
Diameter 32 ''
Length 68 ''.
P&WC: PW545B
Whereas the HTFE-25 (if the info on the brochure is to be believed) gives a thrust of 25kN or 5620lbf and is 1,730mm long and 590mm in diameter.
Diameter 23.23''
Length 68.11 ''.
I couldn't find both the engines' t/w ratio but at a glance the HTFE-25s t/w ratio maybe is better. Or am I wrong?
If HAL can finish it in time, it could be applied in different projects particularly UCAVs.
Correct me if I am wrong but this engine will have civilian application to right?
Nice.
You just said something good about a HAL product
Buddy who the f*ck you are & where is he-man