A rocket has 15,000 kg of fuel and its mass is given by m = 20,000 kg - (50 kg/s)t Thus, its mass will be 12500 kg after 2.5 minutes of flight but it will burn all of its fuel in 5. minutes. A rocket has 15,000 kg of fuel and its mass is given by m = 20,000 kg - (50 kg/s)t. m/s? and its speed will be m/s The exhaust velocity is 4.0 km/s. Starting from rest it fifts-off from the surface of the Earth, After 2.5 minutes of flight its acceleration will be
A rocket has 15,000 kg of fuel and its mass is given by m = 20,000 kg - (50 kg/s)t Thus, its mass will be 12500 kg after 2.5 minutes of flight but it will burn all of its fuel in 5. minutes. A rocket has 15,000 kg of fuel and its mass is given by m = 20,000 kg - (50 kg/s)t. m/s? and its speed will be m/s The exhaust velocity is 4.0 km/s. Starting from rest it fifts-off from the surface of the Earth, After 2.5 minutes of flight its acceleration will be
College Physics
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
Transcribed Image Text:A three stage rocket consists of a first stage that has a total mass of 4,000 kg (3,500 kg of fuel). The second stage has a total mass of 1500 kg (1300 kg of fuel). The third stage has a total mass of 500 kg (400 kg of fuel) The
A rocket has 15,000 kg of fuel and its mass is given by:
m = 20,000 kg - (50 kg/s)t.
Thus, its mass will be 12500
kg after 2.5 minutes of flight but it will burn all of its fuel in 5
minutes.
A rocket has 15,000 kg of fuel and its mass is given by:
m = 20,000 kg - (50 kg/s)t.
The exhaust velocity is 4.0 km/s. Starting from rest it lifts-off from the surface of the Earth. After 2.5 minutes of flight its acceleration will be
m/s? and its speed will be
m/s
A two stage rocket consists of a first stage that has a total mass of 4,500 kg (4,000 kg of fuel). The second stage has a total mass of 1500 kg (1200 kg of fuel). The exhaust velocity is 1.6 km/s If the rocket takes off from rest
km/s when the first stage separates. When the second stage separates the speed of the rocket will be
3.51
km/s. For this rocket to orbit the Earth, the exhaust speed
1.76
then the speed of the rocket will be
would have to be
km/s.
km/s when the first stage separates. When the second stage separates the speed of the rocket will be
exhaust velocity is 1.6 km/s. If the rocket takes off from rest, then the speed of the rocket will be
km/s. For this rocket to orbit the Earth, the exhaust speed would have to be
km/s
km/s. When the third stage separates the speed of the rocket will be
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