Multi-position support structure connecting a payload to a boost

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

Patent

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Details

244172, 410156, B64G 122

Patent

active

052266168

ABSTRACT:
The support structure takes the form of a load isolating payload support strut assembly whose length can be selectively shortened between fully extended and fully compressed to vary the spacing between the payload and the booster rocket during different stages of a flight. The strut assembly would allow independent motion of a separately supported booster rocket and payload during ascent, and subsequently provide a rigid interface during the rocket's flight, which would allow an increase in the capacity of space transferred payloads.

REFERENCES:
patent: 3703998 (1972-11-01), Girard
patent: 4536114 (1985-08-01), Belew

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