Satellite and method to place this satellite in orbit by gravita

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

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244164, 244167, B64G 134, B64G 124

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055074545

ABSTRACT:
Satellite and method for placing said satellite in orbit by lunar gravitational assistance.
After placing the satellite into standard orbit (01) within a quasi-equatorial plane, the satellite is transferred onto a circumlunar orbit (02) so that the satellite traverses the sphere of influence S1 of the moon. On leaving this sphere, the orbit (03) is inside a plane inclined with respect to the equatorial plane. The orbit is then connected to the definitive orbit (04).

REFERENCES:
patent: D100604 (1981-07-01), Crill et al.
patent: 3429526 (1969-02-01), Genty
patent: 3995801 (1976-12-01), Bond
patent: 4288051 (1981-09-01), Goschel
L. M. K. Boelter et al., Space Technology, 1959.
D. G. King-Hele: "An Introduction to Transfer Orbits Technical Note No.: Space 17" Sep. 1962, Royal Aircraft Establishment, Farnborough.
Inter-Electronique, vol. 27, No. 37, 24 Jan. 1972, Paris FR, pp. 14-15 A. Thiboumery: "Le Satellite Europeen HEOS-A2 avant sa mise en orbite".

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