Question: Consider a variant of the Space Shuttle Main Engine ( SSME; RS - 2 5 ) that produces a thrust of 1 . 7 meganewton
Consider a variant of the Space Shuttle Main Engine SSME; RS that produces a thrust of meganewton at sea level. Its specific impulse in a vacuum is The exit diameter of the engine's nozzle is
Calculate how much propellant the engine consumes each second kgs
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