A rocket of mass 5700kg ejects mass at a constant rate of 15kg/s with constant speed of 12km/s. The acceleration of the rocket 1 minute after the blast is
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Thrust = -uR (R is rate of mass ejection)
u is exhaust velocity relative to the rocket
since the gas is travelling at 12000 m/s relative to the rocket
u = - 12000 (opp direction of rocket motion)
after 1 minute mass of rocket = 5700 - 15x60 = 4800 kg
Thrust = -uR = -(-12000)15 = 180000 N (in the direction of rocket motion)
Thrust - 4800g = 4800a
=> 180000 - 4800x10 = 4800a
=> 132000 = 4800a
=> a = 132000 / 4800 = 27.5 m/s²
Ans: acceleration of rocket = 27.5 m/s²
b) Thrust = -uR -------------------------------> (i)
=> Thrust required for initial upward acceleration of 20m/s²
= 5000g + 5000(20) -------------------------> [Fresultant = ma, thrust - w = ma]
= 50000 + 100000 = 150000 N
from (i) => R = -Th./u = -150000/-800
= 1500/8 = 187.5 kg/s
answer is 187.5
Hope this helps you
u is exhaust velocity relative to the rocket
since the gas is travelling at 12000 m/s relative to the rocket
u = - 12000 (opp direction of rocket motion)
after 1 minute mass of rocket = 5700 - 15x60 = 4800 kg
Thrust = -uR = -(-12000)15 = 180000 N (in the direction of rocket motion)
Thrust - 4800g = 4800a
=> 180000 - 4800x10 = 4800a
=> 132000 = 4800a
=> a = 132000 / 4800 = 27.5 m/s²
Ans: acceleration of rocket = 27.5 m/s²
b) Thrust = -uR -------------------------------> (i)
=> Thrust required for initial upward acceleration of 20m/s²
= 5000g + 5000(20) -------------------------> [Fresultant = ma, thrust - w = ma]
= 50000 + 100000 = 150000 N
from (i) => R = -Th./u = -150000/-800
= 1500/8 = 187.5 kg/s
answer is 187.5
Hope this helps you
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