Aerospace Engineering > GATE 2010 > Multi-stage Rockets
A two stage chemical rocket, having the same specific impulse (l9p) of 300 s for both the stages is
designed in such a way that the payload ratio and the structural ratio are same for both the stages.
The second stage of the rocket has following mass distribution:
Propellant Mass=10208 kg
Structural Mass=1134 kg
Payload Mass=1700 kg
gc=9.8 m/s2
If the rocket is fired from rest and it lies in a zero gravity field and a drag free environment, the
final velocity attained by the payload is
A
9729.3 m/s
B
897.3 m/s
C
9360.2 m/s
D
8973.2 m/s

Correct : d

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Related Topics

two stage rocket velocity GATE Aerospace Engineering 2010 GATE AE 2010 Q42 specific impulse rocket equation payload ratio structural ratio rocket mass distribution final velocity of payload aerospace engineering propulsion

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