We describe an interferometric inter-spacecraft ranging system with an expected sensitivity of 1 nm/sqrt(Hz) level or better over frequencies of 10 to 100 mHz. We present our flight system concept and initial breadboard results.
Laboratory demonstration of low Earth orbit inter-satellite interferometric ranging
(CLEO). Conference on Lasers and Electro-Optics, 2005. ; 3 ; 1754-1756 Vol. 3
2005-01-01
2461908 byte
Conference paper
Electronic Resource
English
Laboratory Demonstration of Low Earth Orbit Inter-Satellite Interferometric Ranging
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