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maniacp08
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Gravity Problem -- satellite
A satellite with a mass of 250 kg moves in a circular orbit 8.00 x 10^7 m above the Earth's surface.
(a) What is the gravitational force on the satellite?
N
(b) What is the speed of the satellite?
km/s
(c) What is the period of the satellite?
h
Relevant Equations
gravitational Force = G*m1*m2 / r^2
G = 6.67 x 10^-11 Nm^2/kg^2
The gravitational force is given but I am only given the m1 of the satellite, is m2 the mass of Earth 5.9742 × 10^24 kilograms?
How would I derive the radius from the orbit?
for Part b, I would need the answer for part a right?
for part c:
Would I use this formula to calculate the period?
T^2 = (4pi^2 / G*m) * r^3
A satellite with a mass of 250 kg moves in a circular orbit 8.00 x 10^7 m above the Earth's surface.
(a) What is the gravitational force on the satellite?
N
(b) What is the speed of the satellite?
km/s
(c) What is the period of the satellite?
h
Relevant Equations
gravitational Force = G*m1*m2 / r^2
G = 6.67 x 10^-11 Nm^2/kg^2
The gravitational force is given but I am only given the m1 of the satellite, is m2 the mass of Earth 5.9742 × 10^24 kilograms?
How would I derive the radius from the orbit?
for Part b, I would need the answer for part a right?
for part c:
Would I use this formula to calculate the period?
T^2 = (4pi^2 / G*m) * r^3
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