Passive lateral vibration isolation system for a spacecraft laun

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

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248604, 248636, B64G 122

Patent

active

060126809

ABSTRACT:
A lateral acceleration force isolator that forms a part of an attachment fitting for a payload, such as a spacecraft or satellite, and launch vehicle assembly. An upper portion of the isolator is designed to be attached to the payload and a lower portion is designed to be attached to a launch vehicle. Flexures are positioned in an array between the upper and lower portions to accommodate lateral displacement in the payload attachment fitting, thereby isolating lateral acceleration forces.

REFERENCES:
patent: 2386788 (1945-10-01), Geldhof et al.
patent: 3351307 (1967-11-01), Michel et al.
patent: 3592422 (1971-07-01), Paine
patent: 4211383 (1980-07-01), Starcevic
patent: 4355469 (1982-10-01), Nevins et al.
patent: 4997158 (1991-03-01), James
patent: 5305981 (1994-04-01), Cunningham et al.
patent: 5566919 (1996-10-01), Shephard

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