Attitude and maneuvering corrections require impulses with _________ – McqOptions

MCQOPTIONS

1.	Attitude and maneuvering corrections require impulses with _________ pulse width.
A.	extremely short
B.	extremely large
C.	moderately short
D.	moderately large
Answer» B. extremely large

Discussion

No Comment Found

Related MCQs

Which of the following cannot be the nature of the actuation system for thrust vector control?
For a conical nozzle of throat diameter 0.007 m, exit cross-section diameter 0.02 m, and divergent section length of 0.038 m, determine the nozzle semi-divergence angle.
Which of the following thrust modulation techniques uses a normal shock to reduce total thrust?
Which of the following thrust modulation technique makes use of symmetric injection for jet area control?
Assertion: Oxygen addition in the control flow gases of solid rocket engine will result in a higher characteristic velocity of the exit jet.Reason: Because of secondary combustion, stagnation temperature and pressure increase. Higher stagnation temperature results in exhaust jet characteristic velocity.
Which of the following is not a way for thrust modulation?
Attitude and maneuvering corrections require impulses with _________ pulse width.
Thrust can be varied by changing the throat area along with throttling the flow.
A two-to-one thrust decrease can be achieved using _________ in a liquid propellant rocket engine.
Thrust is a weak function of ______________