- #1
mleesk
- 3
- 0
hello,
does anyone know how to derive the ROCKET ENGINE THRUST formula:
T = P/R AV + (P-B)A
i know you need to use F=ma and Momentum flow rate equations to get the first place. but what do you do after that?
Any help would be greatly appreciated.
Thanks,
Michael
does anyone know how to derive the ROCKET ENGINE THRUST formula:
T = P/R AV + (P-B)A
i know you need to use F=ma and Momentum flow rate equations to get the first place. but what do you do after that?
Any help would be greatly appreciated.
Thanks,
Michael