The patent concerns a system for providing a rocket powered vehicle with complete thrust vectoring capabilities including a convergent-divergent nozzle attached to a motor casing by a flexible joint member. The flexible joint member includes a laminar structure comprising a series of alternate annular elastomeric and metallic shim members. The elastomeric shim members provide omnidirectional flexible capabilities for the nozzle. Integrally connected to the nozzle is a hydraulically controlled pintle member movable along the axis of the nozzle which varies the effective cross-sectional area of the throat of the nozzle and thereby varies the magnitude of the resulting thrust.
Thrust Vectoring Control System for Rocket Nozzles
1971
7 pages
Report
Keine Angabe
Englisch
Aerodynamics Performance Prediction of Thrust-Vectoring Nozzles
Online Contents | 1998
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