A rocket that is in deep space and initially at rest relative to an inertial reference frame has a mass of 2.55* 105 kg, of which 1.81* 105 kg is fuel. The rocket engine is then fired for 250 s while fuel is consumed at the rate of 480 kg/s. The speed of the exhaust products relative to the rocket is 3.27 km/s. (a) What is the rocket’s thrust? After the 250 s firing, what are (b) the mass and (c) the speed of the rocket?

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A: Thrust = Rate of fuel consumption x relative velocity Thrust= 1656x103 N

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Q: Two manned satellites approaching one another at a relative speed of 0.300 m/s intend to dock. The…

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Q: A rocket is at rest in space relative to the Earth and has a total mass (including propellant) of M…

A: Given data The total mass of the rocket is M = 2.55 x 105 kg The fuel consumption rate is m˙f= 480…

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A: Mass of the satellites,

Q: Two manned satellites approaching one another at a relative speed of 0.550 m/s intend to dock. The…

A: Solution:The final relative velocity can be calculated using following steps:Given:

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A: the equation of conservation of momentum,

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A:

Q: Two manned satellites approaching one another at a relative speed of 0.300 m/s intend to dock. The…

A: Given: Relative speed of satellites, urel = 0.300 m/s mass of first satellite, m1 = 2.50 ✕ 103 kg…

Q: A rocket, which is in deep space and initially at rest relative to an inertial reference frame, has…

A:

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Q: Two manned satellites approaching one another at a relative speed of 0.550 m/s intend to dock. The…

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A: Given:- m1 = 2000 kg m2 = 7500 kg

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A: Let u1 be velocity of first satellite and u2 be that of second satelliteAlso , given that masses…

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Q: Find the magnitude of the linear momentum for the following cases. (Enter your answers in (a) a…

A:

Q: Two manned satellites approaching one another at a relative speed of 0.300 m/s intend to dock. The…

A: Given data according to question m1   =    5.50 *  103kg m2   =   7.50 * 103 kg