Aeronautics and astronautics – Aircraft structure – Load accommodation
Patent
1994-02-18
1996-06-25
Kashnikow, Andres
Aeronautics and astronautics
Aircraft structure
Load accommodation
244158R, 244 63, 1022755, 102274, 102378, B64G 122, B64F 104
Patent
active
055292640
ABSTRACT:
A launch vehicle system includes at least one primary solid fuel motor, a shroud for housing a payload and an attitude control system. The attitude control system is connected intermediate the primary solid fuel motor and the shroud. It has a circular outer wall and liquid fuel motors for exerting thrust along a longitudinal axis of the rocket system, and for controlling pitch, roll and yaw of the shroud. The attitude control system includes a support structure defining three pairs of fuel tank supporting zones, each zone having laterally extending supporting brackets connected to the outer wall. The attitude control system also includes connecting tubing for connecting outlets of sets of fuel tanks consisting of one, two and three pairs of fuel tanks to the liquid fuel motors.
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Bedegrew Ernest R.
Chan Allan L.
Connors James J.
Damon Donald E.
Epstein Kenneth W.
Kashnikow Andres
Lockheed Missiles & Space Company Inc.
Mojica Virna Lissi
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