A space vehicle is in a circular orbit of 2200-km radius around the moon. To transfer it
Question:
A space vehicle is in a circular orbit of 2200-km radius around the moon. To transfer it to a smaller circular orbit of 2080-km radius, the vehicle is first placed on an elliptic path AB by reducing its speed by 26.3 m/s as it passes through A. Knowing that the mass of the moon is 73.49 × 1021 kg, determine
(a) The speed of the vehicle as it approaches B on the elliptic path,
(b) The amount by which its speed should be reduced as it approaches B to insert it into the smaller circular orbit.
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For a circular orbit Eq 1228 Then Or V A cire 14930 ...View the full answer
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Related Book For 
Vector Mechanics for Engineers Statics and Dynamics
ISBN: 978-0073398242
11th edition
Authors: Ferdinand Beer, E. Russell Johnston Jr., David Mazurek, Phillip Cornwell, Brian Self
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