Microsatellite system for high-volume orbital telemetry

Optical: systems and elements – Deflection using a moving element – Using a periodically moving element

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359159, H04B 1000

Patent

active

059092998

ABSTRACT:
Detailed mapping of the magnetosphere is made possible by deploying hundreds of attitude-impervious microsatellites, in the form of small corner reflectors with piezoelectric mirror surfaces, from a single mother satellite at spacings of as little as 1 km in equatorial and elliptical orbits. The microsatellites carry magnetosensors whose output is transmitted to a ground station by modulating the reflection of a laser beam transmitted to the microsatellite by the ground station. Various refinements of the laser data link are also disclosed.

REFERENCES:
patent: 3863064 (1975-01-01), Doyle et al.
patent: 5390040 (1995-02-01), Mayeux
patent: 5450223 (1995-09-01), Wagner et al.
patent: 5486833 (1996-01-01), Barrett

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