Explore topic-wise MCQs in Rocket Propulsion.

This section includes 10 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.

How much time does it generally take to start a small thruster with a pressurized feed system?

A. 3-15 ms
B. 1-5 s
C. 3-15 s
D. 1-5 ms
Answer» B. 1-5 s
2.

Which of the following pressurization systems take more time to start for similar engines?

A. Turbopump system
B. Gas pressure feed system
C. Both requires the same time
D. Start time is independent of such systems
Answer» B. Gas pressure feed system
3.

Start delay includes the time taken to _________

A. close valves
B. terminate combustion
C. lower the flow
D. raise chamber pressure
Answer» E.
4.

How is the stable operation of liquid propellant flows achieved?

A. By means of some kind of a pressure feed system
B. By utilizing the gravitational force on the liquids to the rocket s advantage
C. By using suitable pipes and valves which can minimize vibrations
D. Liquid flow system in general are inherently stable
Answer» E.
5.

_________ permits the simulation of operation of critical control components without the actual hot operation of the rocket unit.

A. Checkout controls
B. Safety controls
C. Thrust vectoring control
D. Operating control
Answer» B. Safety controls
6.

In which of the following cases does the electrical valves automatically return to their normal positions?

A. Nonhazardous shutdown
B. Hazardous shutdown
C. Cold start
D. Warm start
Answer» B. Hazardous shutdown
7.

_________ are used to protect personnel and equipment in case of malfunction.

A. Ejection seats
B. Parachute system
C. Rocket casing
D. Safety controls
Answer» E.
8.

Valves, regulators and pressure switches come into picture while considering _________

A. solid rocket engines
B. liquid rocket engines
C. both solid and liquid rocket engines
D. neither solid nor liquid rocket engines
Answer» C. both solid and liquid rocket engines
9.

Single-shot devices are _________

A. devices with a single-engine
B. devices which are deployed only once
C. devices which can fire a single missile
D. colloquial term for missiles
Answer» C. devices which can fire a single missile
10.

The complexity of the control elements of the engine systems depend mostly on _________

A. capital
B. launching site
C. mission
D. trajectory
Answer» D. trajectory