Aircraft/spacecraft ground accelerator

Aeronautics and astronautics – Aircraft propulsion and steering on land or water

Patent

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Details

152310, 244 63, B64F 110

Patent

active

039631966

ABSTRACT:
An accelerator including a framework having an aerodynamic fairing shaped to provide positive pitch and directional stability and including a support and attachment system for holding a fully fueled horizontal takeoff space vehicle such that the negative structure loadings are reduced to a minimum. The running gear system includes a plurality of wheel tire sets with braking and decelerating systems associated therewith.

REFERENCES:
patent: 1686142 (1928-10-01), Bonsieur
patent: 1752845 (1930-04-01), Hibbert
patent: 2774557 (1956-12-01), Jakimiuk et al.
patent: 2877969 (1959-03-01), Dowty
patent: 2921756 (1960-01-01), Borden et al.
patent: 2922602 (1960-01-01), Matheisel et al.
patent: 3208497 (1965-09-01), Schutt
patent: 3210029 (1969-10-01), Brusch et al.
patent: 3437285 (1969-04-01), Manfredi et al.

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