Applications and Investigations in Earth Science (9th Edition)
Applications and Investigations in Earth Science (9th Edition)
9th Edition
ISBN: 9780134746241
Author: Edward J. Tarbuck, Frederick K. Lutgens, Dennis G. Tasa
Publisher: PEARSON
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Question
Problem 2 The following figure shows two satellites in Earth orbits: Satellite A is in a circular orbit with an altitude of 9,622 km, while Satellite B is in an elliptical orbit with an apogee altitude of 9,622 km. At the instant shown in Figure P2, Satellite B is passing through the apogee while Satellite A is ahead of Satellite B with an angular separation of 120 deg. Determine the perigee altitude of the elliptical orbit so that Satellites A and B occupy the same radial position when Satellite A firstly arrives the apogee point (in other words, Satellites A and B perform a rendezvous maneuver at apogee of satellite B).
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Transcribed Image Text:Problem 2 The following figure shows two satellites in Earth orbits: Satellite A is in a circular orbit with an altitude of 9,622 km, while Satellite B is in an elliptical orbit with an apogee altitude of 9,622 km. At the instant shown in Figure P2, Satellite B is passing through the apogee while Satellite A is ahead of Satellite B with an angular separation of 120 deg. Determine the perigee altitude of the elliptical orbit so that Satellites A and B occupy the same radial position when Satellite A firstly arrives the apogee point (in other words, Satellites A and B perform a rendezvous maneuver at apogee of satellite B).
Satellite A 120° Satellite B
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Transcribed Image Text:Satellite A 120° Satellite B
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