A Space ship of mass 5000 kg is heading towards the moon and wants to change its trajectory by 20 degrees relative to original path. The rocket has a velocity of 110 m/s. How much gas must be used up if it burns its rockets (using up fuel) and expels gas at a velocity of 1200 m/s (perpendicular to its direction of motion)?
given,
mass of the rocket = 5000 kg
velocity = 110 m/s ,angle = 20 degree
gases are expelled at speed = 1200 m/s
sideways velocity / radial velocity = tan(20)
Therefore the rocket will have a sideways momentum of
(M-m) * sideways velocity = (M-m) * radial velocity * tan(20)
where, M = initial rocket mass
m = mass of the gas expelled This sideways momentum will be balanced by the momentum of the gases expelled
m *1200 = (5000kg - m) *110* tan(20)
m*1200=200183.62 - 40.36*m
1240.36*m=200183.62
This gives
m = 161.43 kg
mass must be expelled = 161.43 kg
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