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System for imposing directional stability on a rocket-propelled vehicleAn improved system for use in imposing directional stability on a rocket-propelled vehicle is described. The system includes a pivotally supported engine-mounting platform, a gimbal ring mounted on the platform and adapted to pivotally support a rocket engine and an hydraulic actuator connected to the platform for imparting selected pivotal motion. An accelerometer and a signal comparator circuit for providing error intelligence indicative of aberration in vehicle acceleration is included along with an actuator control circuit connected with the actuator and responsive to error intelligence for imparting pivotal motion to the platform. Relocation of the engine's thrust vector is thus achieved for imparting directional stability to the vehicle.
Document ID
19760014187
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Perkins, H.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 8, 2013
Publication Date
April 6, 1976
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
Patent Number: US-PATENT-3,948,470
Patent Application Number: US-PATENT-APPL-SN-493359
Patent Number: NASA-CASE-MFS-21311-1
Accession Number
76N21275
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-3,948,470|NASA-CASE-MFS-21311-1
Patent Application
US-PATENT-APPL-SN-493359
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