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a total load (payload plus? A rocket for use in deep space is to be capable of boosting a total load (payload plus the rocket frame and engine) of 2.9 metric tons to a speed of 10 000 m/s.
(a) It has an engine and fuel designed to produce an exhaust speed of 2 800 m/s. How much fuel plus oxidizer is required?1Your response differs significantly from the correct answer. Rework your solution from the beginning and check each step carefully. metric tons
(b) If a different fuel and engine design could give an exhaust speed of 5 600 m/s, what amount of fuel and oxidizer would be required for the same task?2 metric tonsNoting that the exhaust speed in part (b) is 2.00 times higher than that in part (a), explain why the required fuel mass is not simply smaller by a factor of 2.00.
I have only to 11:00 pm pt please
(a) It has an engine and fuel designed to produce an exhaust speed of 2 800 m/s. How much fuel plus oxidizer is required?1Your response differs significantly from the correct answer. Rework your solution from the beginning and check each step carefully. metric tons
(b) If a different fuel and engine design could give an exhaust speed of 5 600 m/s, what amount of fuel and oxidizer would be required for the same task?2 metric tonsNoting that the exhaust speed in part (b) is 2.00 times higher than that in part (a), explain why the required fuel mass is not simply smaller by a factor of 2.00.
I have only to 11:00 pm pt please