Propulsion, monitoring and control unit particularly for ballist

Details Propulsion, monitoring and control unit particularly for ballist Propulsion, monitoring and control unit particularly for ballist

1988-08-05

1990-01-09

Bentley, Stephen C.

Aeronautics and astronautics

Missile stabilization or trajectory control

Remote control

244120, 102384, F42B 15033

Patent

active

048922684

ABSTRACT:
A command control and propulsion unit for ballistic munitions, including a wind-driven propeller, attached to a front end of the body of the munition for activation of an alternator. The electric power generated by the alternator activates a pump that feeds liquid fuel to a rocket motor oxidized by a liquid oxygen coming from a tank housed in a cradle. The cradle is coupled to a saddle, radially opposite from the cradle, which is provided with hinged and foldable sings. The body of the munition is coupled between the saddle and the cradle.

REFERENCES:
patent: 2423090 (1947-07-01), Fink et al.
patent: 2926611 (1960-03-01), Hinman
patent: 3764091 (1973-10-01), Crowhurst
patent: 4447025 (1984-05-01), Bock et al.
patent: 4553718 (1985-11-01), Pinson

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