College Physics
OER 2016 Edition
ISBN: 9781947172173
Author: OpenStax
Publisher: OpenStax College
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Chapter 8, Problem 37PE
Professional Application
Space probes may be separated from their launchers by exploding bolts. (They bolt away from one another.) Suppose a 4800-kg satellite uses this method to separate from the 1500-kg remains of its launcher, and that 5000 J of kinetic energy is supplied to the two parts. What are their subsequent velocities using the frame of reference in which they were at rest before separation?
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Space probes may be separated from their launchers by exploding bolts. (They bolt away from one another.) Suppose a 5600 kg satellite uses
this method to separate from the 1800 kg remains of its launcher, and that 7000 J of kinetic energy is supplied to the two parts. What are their
subsequent velocities (in m/s) using the frame of reference in which they were at rest before separation? (Assume the final velocity of the
satellite is in the positive direction. Indicate the direction with the sign of your answer.)
Vsatellite
m/s
Viauncher
m/s
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Chapter 8 Solutions
College Physics
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Ch. 8 - Momentum for a system can be conserved in one...Ch. 8 - Professional Application Explain in terms of...Ch. 8 - Can objects in a system have momentum while the...Ch. 8 - Must the total energy of a system be conserved...Ch. 8 - What is an elastic collision?Ch. 8 - What is an inelastic collision? 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