Rocket nozzle for a rocket engine

Details Rocket nozzle for a rocket engine Rocket nozzle for a rocket engine

1989-02-08

1997-04-15

Carone, Michael J.

Power plants

Reaction motor

Including heat exchange means

60266, 23926511, 23926517, F02K 1100

Patent

active

056198515

ABSTRACT:
A diverging rocket engine nozzle has a system to allow ambient gases to flow from the outside to the inside of the nozzle's chamber. The system includes a plurality of coolant conduits adjacent the inside surface of the nozzle. The conduits are spaced apart to provide a plurality of vent openings which extends from the inside to the outside of the nozzle's chamber. A plurality of valves controls gas flow through the vent passages when the pressure outside of the nozzle is greater than the pressure directly adjacent the inside surface of the nozzle. The coolant conduits cool and shield the valves at their points of attachment to the outside of the nozzle.

REFERENCES:
patent: 3469787 (1969-09-01), Marsh et al.
patent: 3563467 (1971-02-01), Marsh et al.
patent: 3712546 (1973-01-01), Kaufmann
patent: 3925982 (1975-12-01), Mueller
patent: 4369920 (1983-01-01), Schmidt

Affiliated with

Also associated with

Rating

Rocket nozzle for a rocket engine does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-353353