Ejectable aerodynamic stability and control

Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C244S003240

Reexamination Certificate

active

07429017

ABSTRACT:
The disclosed system and method for improving aerodynamic stability of aeronautic vehicles generally includes an ejectable grid fin adapted for releasable engagement with aeronautic vehicles. The grid fin is generally configured to optimize the flight performance characteristics of the aeronautic vehicle taken in engaged combination with the grid fin as compared with the flight performance of the aeronautic vehicle taken alone. Disclosed features and specifications may be controlled, adapted or otherwise optionally modified to improve the aerodynamic stability and/or control of a variety of deployed aeronautic vehicles. Exemplary embodiments of the present invention generally provide ejectable grid fins that may be used in conjunction with missiles mounted on an eject rail of an aircraft.

REFERENCES:
patent: 2597703 (1952-05-01), Busacker
patent: 4145017 (1979-03-01), Stiklorus
patent: 4930398 (1990-06-01), Sharples
patent: 5048773 (1991-09-01), Washington et al.
patent: 5642867 (1997-07-01), Klestadt
patent: 6460807 (2002-10-01), Braitinger et al.
patent: 7114685 (2006-10-01), Schulein
Washinton, “AIAA 93-0035” “Grid fins—a new concept for missile stability”, Jan. 11-14, 1993.

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

Ejectable aerodynamic stability and control does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Ejectable aerodynamic stability and control, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Ejectable aerodynamic stability and control will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-3968016

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