Method of loading a solid fuel rocket engine

Details Method of loading a solid fuel rocket engine Method of loading a solid fuel rocket engine

1974-10-29

1976-01-13

Croyle, Carlton R.

Power plants

Reaction motor

Solid propellant

60 3947, 86 1R, 102 99, F02K 904, C06B 2100

Patent

active

039317099

ABSTRACT:
One or both ends of the body of a solid fuel rocket engine is provided with an internally thickened portion, which serves for the mechanical attachment of additional parts, that is the rocket head or the rocket base, to the end of the engine body, without any increase in the external cross-sectional dimension of the body. A block of propellant fuel is located within the engine body and has a portion of reduced cross-sectional dimensions corresponding to the internally thickened portion at the end of the engine body. The block is introduced into the body by cooling the former until its dimensions have shrunk sufficiently for it to be introduced.

REFERENCES:
patent: 3397539 (1968-08-01), Schubert

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