Hybrid rocket propellant with nitroso derivative of hexamethylen

Details Hybrid rocket propellant with nitroso derivative of hexamethylen Hybrid rocket propellant with nitroso derivative of hexamethylen

1965-09-17

1980-06-03

Miller, Edward A.

Explosive and thermic compositions or charges

Structure or arrangement of component or product

Solid particles dispersed in solid solution or matrix

60219, 149 1992, 149 92, C06B 4510

Patent

active

042060060

ABSTRACT:
A rocket fuel is formed by mixing a liquid prepolymer of butadiene having carboxyl groups with hexamethylene tetramine or a nitroso derivative thereof, shaping and hardening.

REFERENCES:
patent: 1720459 (1929-07-01), Wyler
patent: 2997376 (1961-08-01), Bartley
patent: 3066139 (1962-11-01), Zhivadinovich et al.
patent: 3083526 (1963-04-01), Hudson
patent: 3177101 (1965-04-01), Vriesen

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