Method and apparatus for neutralizing the effect of accelerating

Aeronautics and astronautics – Spacecraft – Attitude control

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244121, 244122R, 244122AG, 297216, B64G 100, B64D 1106

Patent

active

041757238

ABSTRACT:
A man-carrying vehicle modified with a device for alleviating accelerative forces particularly useful for space travel is provided with a personnel carrier which automatically orients its occupant, with an imaginary Z-axis parallel to the spinal column and through the centers of mass of cross sections of the body and of the head perpendicular to the Z-axis such that the Z-axis is in a position normal to the resultant of the forces of acceleration, and which rotates the occupant about the Z-axis to alleviate or counteract the effects of the forces of acceleration in the X and Y directions normal to the Z-axis.

REFERENCES:
patent: 2611562 (1952-09-01), Exton, Jr.
patent: 2740599 (1956-04-01), Roberts-Horsfield
patent: 2985413 (1961-05-01), Widmanstetter
patent: 2986361 (1961-05-01), Codding
patent: 3173627 (1965-03-01), Cohen
patent: 3633849 (1972-01-01), Kling
patent: 3826434 (1974-07-01), Beckh
Fraser, "Human Response to Sustained Acceleration," 1966, NASA-SP-103, pp. 1-5, 7-9.

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