System for controlling the nozzle throat area of a rocket motor

Details System for controlling the nozzle throat area of a rocket motor System for controlling the nozzle throat area of a rocket motor

1968-12-23

1976-04-06

Feinberg, Samuel

Power plants

Reaction motor

Condition responsive thrust varying means

F02K 118

Patent

active

039480429

ABSTRACT:
A system for controlling the annular nozzle throat area (and hence the tht) 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.

REFERENCES:
patent: 2566961 (1951-09-01), Poole
patent: 2750734 (1956-06-01), Anxionnaz et al.
patent: 2820340 (1958-01-01), Dolza et al.
patent: 3059425 (1962-10-01), McSherry et al.
patent: 3073112 (1963-01-01), Bleikamp, Jr.

Affiliated with

Also associated with

Rating

System for controlling the nozzle throat area of a rocket motor does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with System for controlling the nozzle throat area of a rocket motor, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and System for controlling the nozzle throat area of a rocket motor will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1568807