- #1
Jacob87411
- 171
- 1
A rocket for use in deep space is to have the capability of boosting a total load (payload plus the rocket frame and engine) of 3.10 metric tons to a speed of 10 000 m/s.
(a) It has an engine and fuel designed to produce an exhaust speed of 2800 m/s. How much fuel plus oxidizer is required?
(b) If a different fuel and engine design could give an exhaust speed of 4600 m/s, what amount of fuel and oxidizer would be required for the same task?
I honestly have no idea where to even start because this hasnt been gone over in class or in the book, so if anyone could just give me a basic idea of how to approach it it would be helpful
(a) It has an engine and fuel designed to produce an exhaust speed of 2800 m/s. How much fuel plus oxidizer is required?
(b) If a different fuel and engine design could give an exhaust speed of 4600 m/s, what amount of fuel and oxidizer would be required for the same task?
I honestly have no idea where to even start because this hasnt been gone over in class or in the book, so if anyone could just give me a basic idea of how to approach it it would be helpful