Explore topic-wise MCQs in Rocket Propulsion.

This section includes 9 Mcqs, each offering curated multiple-choice questions to sharpen your Rocket Propulsion knowledge and support exam preparation. Choose a topic below to get started.

1.

Precise control of engine performance parameters via the use of an automatic feedback system employing a digital computer for control purposes is _________ compared to static calibration of the engine design.

A. simpler
B. complex
C. equally difficult
D. unachievable
Answer» C. equally difficult
2.

The gas pressure in the propellant tank is _________

A. unregulated pressure
B. sea level pressure
C. ambient pressure
D. regulated pressure
Answer» E.
3.

In a pressurized feed system, the pressurizing gas is supplied from its high-pressure tank through ____ for the pressurization of both fuel and oxidizer.

A. regulator
B. passage valves
C. expansion joints
D. combustion chamber
Answer» B. passage valves
4.

The calibration procedure for turbopump system is ___________ complex compared to gas pressure fed systems.

A. equally
B. less
C. more
D. unrelated
Answer» D. unrelated
5.

The operating mixture ratio is usually ________

A. fuel-rich
B. fuel-lean
C. oxidizer-rich
D. doesn’t matter
Answer» B. fuel-lean
6.

Under ideal conditions, the ratio of the rated flows has to be _________ desired mixture ratio.

A. Equal to
B. less than
C. more than
D. unrelated to
Answer» B. less than
7.

Which of the following forces on a rocket engine is more significant than the rest of them?

A. Actuator forces
B. Maneuver forces
C. Vibration forces
D. Thrust load
Answer» E.
8.

The process of balancing the pressure available to the engine against the pressure drop plus the chamber pressure is called as __________

A. chamber balance
B. engine balance
C. pressure balance
D. overall balance
Answer» D. overall balance
9.

The calibration procedure for the turbopump system is ________ complex compared to gas pressure fed systems.

A. equally
B. less
C. more
D. unrelated
Answer» D. unrelated