PROBLEM 14.10
For the satellite system of Prob. 14.9, assuming that the
velocity of the base satellite is zero, determine (a) the position
vector r of the mass center G of the system, (b) the linear
momentum mv of the system, (c) the angular momentum HG
of the system about G. Also, verify that the answers to this
problem and to Prob. 14.9 satisfy the equation given in Prob.
14.27.
PROBLEM 14.9 A 20-kg base satellite deploys three sub-
satellites, each which has its own thrust capabilities, to
perform research on tether propulsion. The weights of sub-
satellite A, B, and C are 4 kg, 6 kg, and 8 kg, respectively, and
their velocities expressed in m/s are given by vA = 4i – 2j +
2k, vB = i + 4j, vC = 2i + 2j + 4k. At the instant shown, what
is the angular momentum HO of the system about the base
satellite?