A 5000 kg rocket is set for vertical firing. The exhaust speed is 800 ms−1. To give an upward acceleration of 20 ms−2, the amount of gas ejected per second to supply the needed thrust is
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Given :-
Mass of rocket = m = 5000 Kg
Velocity of rocket = u = 800 ms-¹
Acceleration of rocket = a = 20 ms-²
Acceleration due to gravity = g = 10 ms-²
As we know that by a relation When a body goes upward.
F = m(g+a)/u
F = 5000(10+20)/800
F = 50 × 30/8
F = 187.5 Kgs-¹.
Hence,
Amount of gas ejected = F = 187.5 Kgs-¹.
Some other information :-
This question is related to apparent weight of object in air.
When the body accelerates upward, the apparent weight of the body increases.
R - mg = ma
R = ma + mg
R = m(a + g).
Here, acceleration is in upward direction and acceleration due to gravity is acting in downward direction.
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