Anti-missile missile

Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control

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244158, F41G 900

Patent

active

041098838

ABSTRACT:
An anti-missile missile employing an accelerator of the Van de Graaff or linear type which is carried by the missile to propel particles, such as gamma aluminum oxide, at hypervelocities, the particles being as small as about 10.sup.-7 cm in diameter.

REFERENCES:
patent: 2783684 (1957-03-01), Yoler
patent: 3036213 (1962-05-01), Dessler et al.
patent: 3086424 (1963-04-01), Lio
patent: 3131300 (1964-04-01), Jeter et al.
patent: 3153367 (1964-10-01), Ross et al.
patent: 3239712 (1966-03-01), Norris
"Anti-Satellite Techniques Investigated", Aviation Week, 10/3/60, pp. 54, , 57, 59, 63.

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