Earth orbiting satellite having electrical energy storage batter

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

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244 57, 244173, B64G 144, B64G 122, B64D 3310

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056346123

ABSTRACT:
A three axis stabilized geostationary satellite comprises a structure having walls that face North and South when the satellite is on station and carrying at a storage battery of large capacity. The storage battery is constituted by cells mounted on a chassis having a base plate oriented North-South and mechanically secured to sides that face North and South when the satellite is on station. The sides carry thermal radiators that are thermally connected to each other and to the cells. Typically sides are in alignment with North and South faces of the structure and extend away from the Earth.

REFERENCES:
patent: 3830663 (1974-08-01), Eisele et al.
patent: 4580748 (1986-04-01), Dalby
patent: 4735382 (1988-04-01), Pinson
patent: 5310141 (1994-05-01), Homer et al.
Journal of Powersources - vol.18, No. 2-3, Sep. 1986, Lausanne, CH-pp. 245-258-Metcalfe, J. "Lightweight, Direct-Radiating Nickel-Hydrogen Batteries" - whole document -.
21st Intersociety Energy Conversion Engineering Conference vol. 3 Aug. 29, 1986, San Diego, California, USA pp. 1541-1546? Wong et al. "Intelsat VI Nickel-Hydrogen Battery"-Whole document.

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