A space shuttle is in a circular orbit at a height of 250km, where the acceleration of Earth’s gravity is 93% of its surface value. What is the period of its orbit?
Radius of Earth,
Altitude of the satellite, h= 2.5*105m
Radius of Orbit, R=Re + h = 6.6281*106m
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Centripetal acceleration,
Given that the acceleration of Earth’s gravity is 93% of its surface value.
0.93g = v2 /R
0.93g*R = v2
0.93 * 9.81m/s2 * 6.6281*106m = v2
Orbital velocity, v=7776.255 m/s
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Orbital velocity,
T =( 2** 6.6281*106 )/7776.255m/s
T= 5355.48s
ANSWER: 1.4876 hr
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