In: Physics
Two manned satellites approaching one another at a relative speed of 0.300 m/s intend to dock. The first has a mass of 4.00 ✕ 103 kg, and the second a mass of 7.50 ✕ 103 kg. Assume that the positive direction is directed from the second satellite towards the first satellite.
(a) Calculate the final velocity after docking, in the frame of
reference in which the first satellite was originally at
rest.
??????m/s
(b) What is the loss of kinetic energy in this inelastic
collision?
??????J
(c) Repeat both parts, in the frame of reference in which the
second satellite was originally at rest.
final velocity
??????m/s
loss of kinetic energy
??????J
Given that satellites approach one another at a relative speed of 0.300 m/sec
u2 - u1 = 0.300 m/sec
Which means relative to 1st satellite, 2nd satellite is moving at 0.300 m/sec and at this moment speed of 1st satellite is at rest
u1 = 0 and u2 = 0.300 m/sec
for inelastic collision we know that
Pi = Pf
m1*u1 + m2*u2 = (m1 + m2)*V
V = (m1*u1 + m2*u2)/(m1 + m2)
m1 = mass of 1st satellite = 4000 kg, & m2 = 7500 kg
So Using above values:
V = (4000*0 + 7500*0.300)/(4000 + 7500)
V = 0.19565 m/s
Part B.
loss in kinetic energy will be given by:
dKE = KEi - KEf
dKE = (1/2)*m1*u1^2 + (1/2)*m2*u2^2 - (1/2)*(m1 + m2)*V^2
Using given values:
dKE = (1/2)*4000*0^2 + (1/2)*7500*0.300^2 - (1/2)*(4000 + 7500)*0.19565^2
dKE = 117.4 J = KE lost
Part C.
Now in the same reference frame, when 2nd satellite was originally at rest, in other words, u2 - u1 = -0.300 m/sec
where u2 = 0 & u1 = -0.300 m/sec
for inelastic collision we know that
Pi = Pf
m1*u1 + m2*u2 = (m1 + m2)*V
V = (m1*u1 + m2*u2)/(m1 + m2)
m1 = mass of 1st satellite = 4000 kg, & m2 = 7500 kg
So Using above values:
V = (4000*(-0.300) + 7500*0)/(4000 + 7500)
V = -0.10435 m/s = final velocity
loss in kinetic energy will be given by:
dKE = KEi - KEf
dKE = (1/2)*m1*u1^2 + (1/2)*m2*u2^2 - (1/2)*(m1 + m2)*V^2
Using given values:
dKE = (1/2)*4000*(-0.300)^2 + (1/2)*7500*0^2 - (1/2)*(4000 + 7500)*(-0.10435)^2
dKE = 117.4 J = KE lost