Propulsion, monitoring and control unit particularly for ballistic objects
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United States of America Patent
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-
Jan 9, 1990
Grant Date -
N/A
app pub date -
Aug 5, 1988
filing date -
Aug 5, 1988
priority date (Note) -
Expired
status (Latency Note)
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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.
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