Skip to main content
Exam
Vibe
About Us
Engineering
Aerospace Engineering
Biomedical Engineering
Chemical Engineering
Civil Engineering
Computer Science
Digital Marketing Quiz
Electrical Engineering
Electronics and Communication Engineering
Mechanical Engineering
Govt Exam
Banking Exams
Other Government Exam Preparations
Police
Railway Exams
SSC
State PSC Exams
Teaching / Education Exams
UPSC Exams
Blog
Contact
Search MCQs
🔍
Login
Register
Home
›
Aerospace Engineering
›
Rocket Propulsion MCQ
›
The thrust produced by a rocket is given by:
The thrust produced by a rocket is given by:
A. Mass flow × exhaust velocity + pressure difference term
B. Lift × drag
C. Weight × velocity
D. Fuel mass × altitude
Explanation:
Thrust = ṁ × ve + (pe – pa)Ae.
« Previous
Next »
More from Rocket Propulsion MCQ:
The main limitation of nuclear thermal rockets is:
Which rocket engine was used in the Saturn V first stage?
Electric propulsion systems have:
Which loss is most significant in chemical rockets?
The nozzle used in rockets is generally:
The O/F ratio in rocket propulsion refers to:
The main advantage of liquid rocket engines is:
Ion thrusters work on the principle of:
The staging of rockets is used to:
In vacuum, rocket efficiency is:
Latest Blogs
NEW
CBSE 12th Result 2026 Re-Evaluation: Apply Online, Fees, Last Date & Step-by-Step Process Explained
NEW
NEET UG 2026 Re-Exam Date Announced: Check New Exam Date, Schedule & Latest Updates
NEW
Understanding the SSC Phase 14 Exam: A Comprehensive Overview
NEW
Top Study Tips for Cracking Your Exams with Confidence
NEW
Aerospace Engineering: Scope, Courses & Career Opportunities
NEW
SSC CHSL Syllabus
NEW
EPFO 3.0 is Here: 7 Major Changes Every Employee Must Know
NEW
Indian Army Salary Structure
NEW
Java Interview Questions
NEW
SSC CHSL 2025: Revised Exam Dates, Important Instructions & Study Strategy
NEW
How to Prepare for SSC CGL in 3 Months
NEW
Top 10 Engineering Exams After 12th