Booster rocket range safety system

Ammunition and explosives – Having reaction motor – Having separation means

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Details

89 114, 244172, F42B 1538

Patent

active

051177587

ABSTRACT:
In response to an abort command, fragmentation of a propellant booster rot carried on a missile is limited by positioning of annular shaped charges at axially spaced locations on the outer shell of the booster rocket. Detonation of the charges thereby severs an intermediate section of the rocket from forward and aft sections which remain attached to the missile. The intermediate section is separated from the missile by such severing action to prevent further fragmenting forces from being imparted thereto.

REFERENCES:
patent: 3048107 (1962-08-01), Samms
patent: 3218973 (1965-11-01), Hallum
patent: 3244104 (1966-04-01), Mills et al.
patent: 3903803 (1975-09-01), Losey
patent: 4452412 (1984-06-01), von Pragenau
patent: 4649824 (1987-03-01), Guay
patent: 4685376 (1987-08-01), Noel et al.

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