Spin nozzle and thrust augmentor mechanism

Details Spin nozzle and thrust augmentor mechanism Spin nozzle and thrust augmentor mechanism

1975-11-10

1977-02-15

Croyle, Carlton R.

Power plants

Reaction motor

Rotating or cyclic movement during axial thrust

60271, 23926517, 244 323, F02K 124

Patent

active

040075869

ABSTRACT:
A spin nozzle system for imparting a thrust to pre-spin a missile prior to aunching. This system includes locating the spin nozzles within the outside diameter of the main missile motor. Also the nozzle exhaust gases are exited into the main motor exhaust cone to thereby augment the total missile thrust.

REFERENCES:
patent: 2518002 (1950-08-01), Goddard
patent: 2523011 (1950-09-01), Goddard
patent: 2968996 (1961-01-01), Strickland et al.
patent: 3166897 (1965-01-01), Laurence et al.
patent: 3481543 (1969-12-01), Lovingham

Affiliated with

Also associated with

Rating

Spin nozzle and thrust augmentor mechanism does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Spin nozzle and thrust augmentor mechanism, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Spin nozzle and thrust augmentor mechanism will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1431907