Asymmetric side-exhausting nozzles

Details Asymmetric side-exhausting nozzles Asymmetric side-exhausting nozzles

1986-07-14

1987-03-03

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

23926511, 23926519, F42B 15033, B63H 1112

Patent

active

H00002364

ABSTRACT:
Asymmetric side exhausting nozzles are provided for exhausting propulsion ses of a rocket to the side of the rocket to provide a performance gain of from 1 to three percent over axis symmetric side exhausting nozzles.

Affiliated with

Also associated with

Rating

Asymmetric side-exhausting nozzles does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Asymmetric side-exhausting nozzles, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Asymmetric side-exhausting nozzles will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1008575