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Autonomous rendezvous and docking in synchronous orbit with a 10.6-μm ladar

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Abstract

Recent studies conducted under NASA auspices have established that a pulsed CO2 ladar will offer a cost-effective and reliable solution to a family of space rendezvous and docking requirements. In addition, a system has been configured that is capable of performance unattainable by any other means.

© 1976 Optical Society of America

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