Yeah, it was like 11 o'clock where I live. You're lucky I was still forming coherent scentences by that time .
This thread make me think of something: The F16 is unique as, if I'm understanding correctly, it's thrust at burner actually eXCEEDS the weight of the jet? So...it can accelerate going straight up. What propeller-driven craft has come closest to that?
Any helicopter.HiTech
FYI the F15's had a much higher than 1 -1 thrust to weight ratio.Could go from deck to 60k straight up on afterburner.From WikiFightersF15C 46,900 (2) each engine each producing 46,900 lbs of thrust.Aircraft weight, full fuel, 51,023Max takeoff load 81,000Thrust to weight full fuel 1.14As fuel burned it would just get better.F-15K F-15C Mig-29K Mig-29B F-221.14 1.03 1.00 1.15 1.14I believe the F14 would do similar.
I was coherent, I was just confusing my terms by that time. If I had made that post at, say, 8 o'clock, I would have said "thrust to weight ratio of 1:1".After about 10, I can't think strait, and after 11, I'm lucky to make any sense what so ever.
Ok now I am confused? What produces thrust or in this case more thrust if not the engine?? I are NOT an engineer
Thrust is controlled by raising or lowering the revolutions-per-minute (rpm) of the engine by using the throttle.
Or by increase toque on the prop along with increasing the pitch of the prop. I.E. constant speed props.HiTech