Load-reducing rocket nozzle operation method

Ordnance – Rocket launching – Underwater launching

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

89 11, F41F 307

Patent

active

051157101

ABSTRACT:
A submarine launched missile generates undesirable stress on the rocket nle hydraulic control system at the moment of ignition of the rocket motor. This stress can be minimized by operating the system so that the nozzle is near center and the hydraulic actuator valves are open at ignition.

REFERENCES:
patent: 3166977 (1965-01-01), Pickett et al.
patent: 3166979 (1965-01-01), Draim
patent: 4671163 (1987-06-01), Erikson
patent: 4949618 (1990-08-01), Tarlano

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Load-reducing rocket nozzle operation method does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Load-reducing rocket nozzle operation method, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Load-reducing rocket nozzle operation method will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-412385

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.