Dynamics 2e 855
Problem 5.6
The spacecraft shown is out in space and is far enough from any other mass (e.g., planets, etc.) so as not to
be affected by any gravitational influence (i.e., the net external force on the rocket is approximately zero).
The system (i.e., the spacecraft and all its fuel) is at rest when it starts at
A
, and it thrusts all the way to
B
along the straight line shown using internal chemical rockets (which work by ejecting the fuel mass at very
high speeds out the tail of the rocket). We are given that the mass of the system at
A
is
m
and that it has
ejected half of its mass in thrusting from
A
to
B
. What will be the location of the system’s mass center
when the spacecraft reaches B?
Solution
of McGraw-Hill, and must be surrendered upon request of McGraw-Hill. Any duplication or distribution, either in print or electronic form, without the
permission of McGraw-Hill, is prohibited.