Rocket motor comprising combustible case, nozzle, and fins

Details Rocket motor comprising combustible case, nozzle, and fins Rocket motor comprising combustible case, nozzle, and fins

1977-11-04

1978-10-10

Feinberg, Samuel

Ammunition and explosives

Igniting devices and systems

60200A, F42B 1510

Patent

active

041190360

ABSTRACT:
A combustible rocket is constructed with a laminate which comprises high tensile strength metal foils, easily combustible metal foils, and easily combustible adhesive layers. The rocket has sufficient mechanical strength and its shell can be gasified or disintegrated into finely divided pieces after the propellant of the rocket has burnt out at high altitudes. This rocket can be launched safely even in the vicinity of population centers without risk of injury to living things.

REFERENCES:
patent: 2977885 (1961-04-01), Perry et al.
patent: 3032970 (1962-05-01), Fox
patent: 3127739 (1964-04-01), Miller
patent: 3326129 (1967-06-01), Gould

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