Stage separation mechanism for space vehicles

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

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Details

102378, B64G 164

Patent

active

053182553

ABSTRACT:
A mechanism locking and controllably releasing two space vehicles along a preselected separation axis. The mechanism including a mechanical lock/release and a spring separation device that controllably forces the two space vehicles apart. An electrical interconnect maintains electrical communication between the two space vehicles when locked together. The two space vehicles can be reliably separated by activating a single disengagement actuator.

REFERENCES:
patent: 3116895 (1964-01-01), Mitchum, Jr.
patent: 3122098 (1964-02-01), Glennan
patent: 3174706 (1965-03-01), Wagner
patent: 3352192 (1967-11-01), Webb
patent: 3420470 (1969-01-01), Meyer
patent: 4715565 (1987-12-01), Wittmann
patent: 5108049 (1992-04-01), Zinovi

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