Given: G = 6.67259 × 10−11 Nm2/kg2 The acceleration of gravity on the surface of a planet of radius R = 7770 km is 12.6 m/s2. What is the period T of a satellite in circu- lar orbit h = 10800.3 km above the surface? Answer in units of s. *note:*(must convert distance to meters)
\[mg = G\frac{ mM }{R^2 }\]
\[g = G\frac{ M }{R^2 }\] \[12.6=6.67259 × 10^{−11}\frac{ M }{(7700*1000)^2 }\]
I dont have mass thats the part that is tripping me up lol
find M, the mass of the planet, and use in: \[\frac{ V^2 }{ r} = G\frac{ M }{ r^2 }\] (where r is the radius of the orbit) in order to find V. from V, period is easy to find...
V=\[\sqrt{gr}\]
then i took that and used T=2piR/V
then T/3600
should i have divided by something else to get my period? I:
doesn't work that way
the value given for 'g' is only valid on the planet's surface
it's a crazy fact about gravity that the force of attraction two masses experience is dependent on the inverse square of the distance between them.... if you were on the moon, do you think you would experience an acceleration of 9.8 m/s^2 towards the earth?
this is universal gravitation
so g is constant for all space, is that what you're saying? ... cool.
can i try to solve it
actually my equation editor is not working now. its a big problem
note that \(g=\frac{GM}{r^2}\) g=12.6, G is given, R is 7770000m. I think you can find the M......
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