Method of placing a geostationary telecommunicaiton satellite in

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

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244165, B64G 120

Patent

active

050676725

ABSTRACT:
A geostationary telecommunication satellite has a platform pointed towards the sun and a payload that is rotatable so as to point always toward the Earth. A method of placing this satellite in its final orbit entails using the inertia wheel of the satellite together with its sensors and possibly its two-axis rate gyro to secure attitude control of the satellite during the transfer, that is while in the transfer orbit and during the apogee burn.

REFERENCES:
patent: 2973162 (1961-02-01), Haeussermann
patent: 4306692 (1981-12-01), Kaplan et al.
patent: 4508297 (1985-04-01), Mouilhayrat et al.
Briggs et al., Electrical Power Subsys. for INSAT-1 Conference "Energy to 21 Century" Aug. 18-22, 1980, pp. 1058-1063.

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