Missile system

Ammunition and explosives – Igniting devices and systems

Patent

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Details

F42B 1510

Patent

active

041310659

ABSTRACT:
A missile system with geometric constraints having a plurality of booster ages in tandem and carrying a segmented payload which is situated in the annular area between the last stage booster motor, which is smaller in diameter than the booster motors of preceding stages, and the missile skin.

REFERENCES:
patent: 3170655 (1965-02-01), Pierce
patent: 3260204 (1966-07-01), Wilkey, Jr.

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