Two satellites S1 and S2 revolve round a planet in coplanar circular orbits in the same sense. Their periods of revolution are 1 hour and 8 hours respectively. The radius of the orbit of S1=104km When S2 is closest to S1 find speed of S2 relative to S2 and the angular speed of S1 actually observed by an astronaut at S1.
∵T2∝r3
Given r1=104km = 107m,T1 = 1 hour and T2 = 8 hours.
Therefore, r32=(107)3×(81)2=64×1021
or r2=4×107m=4×104km
(a) The orbital speeds of satellites S1 and S2 respectively are
v1=2πr1T1=2π×1041=2π×104km/h our
And v2=2πr2T2=2π×4×1048=π×104km/h our
The magnitude the speed of S2 relative to
S1 is |v2−v1|=π×104=3.14×104 km/h our
The angular speed of S2 relative to S1 is
ω=v2−v1(r2−r1)=−3.14×104(4×104−104)=−3.143
= −3.143=3.143=−160×160
= -2.91 ×10−4 rad s−1
The negative sign indicates that the sense of rotation of opposite to the sense of revolution of the satellites.