Free return lunar flyby transfer method for geosynchronous satel

Aeronautics and astronautics – Spacecraft – Spacecraft formation – orbit – or interplanetary path

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B64G 110

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06116545&

ABSTRACT:
A method is provided for using a lunar flyby maneuver to transfer a satellite from a quasi-geosynchronous transfer orbit having a high inclination to a final geosynchronous orbit having a low inclination. The invention may be used to take the inclination of a final geosynchronous orbit of a satellite to zero, resulting in a geostationary orbit, provided that the satellite is launched in March or September.

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Rudolf Meyer, Elements of Space Technology for Aerospace Engineers, Academic Press, pp 61-95, 1999.
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"Use of the Moon's Gravitational Field to Inject a Space Vehicle into a Stationary Earth-Satellite Orbit", Ivashkin et al. Kosmicheskie Issledovaniya, vol. 9, No. 2, pp. 163-172, Mar.-Apr. 1971.
Kawaguchi et al., "On Making Use of Lunar and Solar Gravity Assists in Lunar-A, Planet-B Missions," Acta Astronautica, vol. 35, No. 9-11, pp. 633-642, 1995.
Belbruno et al., "Sun-Perturbed Earth-to-Moon Transfers with Ballistic Capture," Journal of Guidance, Control and Dynamics, vol. 16, No. 4, Jul.-Aug. 1993.
Belbruno et al., "Ballistic Caputure Lunar Transfer Determination for the US Air Force Academy Blue Moon Mission," AAS/AIAA Space Flight Mechanics Meeting, Feb. 10-12, 1997.

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