Secondary-injection thrust vector control systems.
Fluidic secondary injection thrust vector control systems for solid propellant and hydrogen-oxygen rocket engines
Rivard, J. G.↗
Engineering topics
Rivard, J. G.
Publications and source records attributed to Rivard, J. G..
Study of vortex valve for medium temperature solid propellants
Fluid state vortex valve secondary injection control system shows considerable promise for future application to solid propellant rocket engine thrust vector control. The single axis injection system tested would be capable of providing secondary injection thrust vector control using 2000 deg F gas.
Holt, W. D.↗
Research study of the vortex valve for medium-temperature solid propellants
Fluid state control system with vortex valves for solid propellant gas generator flow throttling
THROTTLING↗
Development of an all-fluid amplifier for liquid rocket applications Final report
Vortex amplifier for controlling secondary flow for thrust vector control of liquid rocket engine
LIQUID PROPELLANT ROCKET ENGINE↗