One modified RS-25 engine produces 2 Mega Newtons of thrust. The Specific Impulse for the rocket engine is 408 s. Calculate the masses of liquid oxygen and hydrogen for a first stage burn time of 515 seconds using 4 of these RS-25 engines.
One modified RS-25 engine produces 2 Mega Newtons of thrust. The Specific Impulse for the rocket engine is 408 s. Calculate the masses of liquid oxygen and hydrogen for a first stage burn time of 515 seconds using 4 of these RS-25 engines.
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One modified RS-25 engine produces 2 Mega Newtons of thrust. The Specific Impulse for the rocket engine is 408 s.
Calculate the masses of liquid oxygen and hydrogen for a first stage burn time of 515 seconds using 4 of these RS-25 engines.
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