Consider a rocket taking off from the surface of the Moon. The rocket has two engines with identical Isp, connected to a single propellant system.
If one engine fails, which factor will be the most directly affected?
Propellant fraction
Exhaust velocity
Thrust-to-weight ratio
Gross takeoff weight
Answers
Answered by
1
Explanation:
Gross takeoff weight.
Hence, the option (iv) is correct.
Answered by
0
Answer:
Explanation:
Thrust to weight ratio is the correct answer
Similar questions