GATE AE · 2024 · AE
Question 57: Rockets
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Question 57
AENAT2 marksNeeds review
A chemical rocket with an ideally expanded flow through the nozzle produces
thrust at sea level. The specific impulse of the rocket is 200 s and acceleration due to gravity at the sea level is
. The propellant mass flow rate out of the rocket nozzle is ________ kg/s (rounded off to the nearest integer).Log in to check the answer
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2024AE
GATE AE 2024 · Paper 1
Aerospace Engineering · Original paper archive
- Section
- Aerospace Engineering
- Question type
- Numerical answer (NAT)
- Marks
- 2 marks
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