Liquid fuel multistage rocket

Ammunition and explosives – Igniting devices and systems

Patent

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Details

60 3948, 60259, F02C 312

Patent

active

039345122

ABSTRACT:
This invention is a rocket which has a thrust stage located at the lowermost stage and an arbitrary number of propellant stages which are cut off in turn from a propellant stage located at the uppermost stage after exhausting fuel therein.

REFERENCES:
patent: 2686473 (1954-08-01), Vogel
patent: 3048107 (1962-08-01), Samms
patent: 3067682 (1962-12-01), Feldmann et al.
patent: 3199455 (1965-08-01), Samms
patent: 3202381 (1965-08-01), Wuenscher
patent: 3218974 (1965-11-01), Samms
patent: 3384016 (1968-05-01), Blanchard, Jr.
patent: 3534686 (1970-10-01), Watson

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