Hi, I'm stuck on this problem:
A space shuttle orbits earth in a near-circular orbit at a constant speed approximately 100 miles above the Earth's surface.
If we assume that the centripetal acceleration is equal to the acceleration due to gravity at sea level (9.8 m/s^2) and the orbital radius is equal to the radius of the Earth (6380 km):
a) what is the average speed of the shuttle?
b) How long does it take the shuttle to make one orbit around earth?
I'm specifically having problems w/ the wording on the first sentence, is 100m the speed of the shuttle or is it the distance above earth?
is it:
...at a constant speed 100 miles, above the earth's surface...
or
...at a constant speed, 100 miles above the earth's surface.
- in any case how would i go about solving it?
2007-02-06
17:00:22
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3 answers
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asked by
Anonymous
in
Science & Mathematics
➔ Physics
I know that for circular motion:
Acceleration = (Velocity^2)/ Radius
2007-02-06
17:01:45 ·
update #1