Free return lunar flyby transfer method for geosynchronous satel

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

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701226, B64G 110

Patent

active

061491039

ABSTRACT:
A method is provided for using at least two lunar flyby maneuvers 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, through the use of a first leading-edge lunar flyby and subsequent successive leading or trailing edge lunar flybys resulting in a geostationary orbit.

REFERENCES:
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patent: 5507454 (1996-04-01), Dulck
patent: 5511748 (1996-04-01), Scott
patent: 5716029 (1998-02-01), Spitzer et al.
Rudolf Meyer, Elements of Space Technology for Aerospace Engineers, Academic Press, pp. 61-95, 1999.
Oberg, J. E. "Star Wars: Pearl Harbor in Space", Jul. 1984, OMNI Magazine, pp. 42-73.
"Geostationary Orbits From Mid-Latitude Launch Sites Via Lunar Gravity Assist", Graziani et al., Spaceflight Dynamics Vol. 84, Part I, 1993, pp. 561-572.
"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.

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