This report describes a thrust vector control system for rockets that use a solid protrusion inserted into the exit cone of the rocket nozzle. This protrusion is inserted linearly into one side of the rocket exit nozzle and creates a side force for use in control of the missile in flight.
Solid Protrusion Jet Vector Control System
1979
7 pages
Report
Keine Angabe
Englisch
Rocket Engines & Motors , Hydraulic & Pneumatic Equipment , Government Inventions for Licensing , Patent applications , Thrust vector control systems , Control rods , Rocket nozzles , Exits , Walls , Protuberances , Retractable , Fluidic control , Modulators , Pulse duration modulation , Protrusions
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