Exam
Vibe
Home
Engineering
Aerospace Engineering
Biomedical Engineering
Chemical Engineering
Civil Engineering
Computer Science
Electrical Engineering
Electronics and Communication Engineering
Mechanical Engineering
Govt Exam
Banking Exams
Other Government
Police
Railway Exams
SSC
State PSC Exams
Teaching / Education Exams
UPSC Exams
Blog
Contact
๐
Home
โบ
Aerospace Engineering
โบ
Rocket Propulsion MCQ
โบ
The nozzle used in rockets is generally:
The nozzle used in rockets is generally:
A. Convergent only
B. Convergent-divergent (de Laval nozzle)
C. Straight tube
D. Flat plate
Explanation:
Rocket engines use convergent-divergent nozzles to accelerate exhaust gases.
Tags:
Rocket Propulsion MCQ
,
Aerospace Engineering
ยซ Previous
Next ยป
More from Rocket Propulsion MCQ:
The main principle behind rocket propulsion is:
The exhaust velocity of a rocket depends on:
The specific impulse of a rocket engine is defined as:
Which type of propulsion system uses both liquid fuel and oxidizer?
Solid rocket motors are commonly used because they:
The main disadvantage of solid rocket motors is:
Explore more in Aerospace Engineering:
Aerodynamics MCQs MCQs
Flight Mechanics MCQ MCQs
Aircraft Structures MCQs
Propulsion MCQ MCQs
Avionics MCQ MCQs
Aircraft Design MCQs
Spacecraft Engineering MCQ MCQs
Orbital Mechanics MCQ MCQs
Aerospace Materials MCQ MCQs
Flight Testing MCQ MCQs