The patent relates to a system for controlling the annular nozzle throat area (and hence the thrust) of a solid-propellant rocket by means of a pintle or plug the position of which is caused to vary in response to pressure variations within the combustion chamber of the rocket.
System for Controlling the Nozzle Throat Area of a Rocket Motor
1968
5 pages
Report
No indication
English
Annular throat rocket nozzle design
TIBKAT | 1961
|Biaxial Fracture Behavior of Graphite for Nozzle Throat Insert of Solid Rocket Motor
British Library Conference Proceedings | 2002
|