Matches 1 - 10 out of 10


Match Document Document Title
US20120048993 AERODYNAMIC FLIGHT TERMINATION SYSTEM AND METHOD  
A missile has a flight termination system that includes deployable lift surfaces that deploy forward of a center of gravity of the missile. When deployed, the lift surfaces cause the missile to...
US20090090809 METHOD OF INCREASING THE RANGE OF A SUBCALIBRE SHELL AND SUBCALIBRE SHELLS WITH LONG RANGE  
The invention relates to a method for increasing the range of shells (1, 8, 13) charged with an explosive substance and other types of shell, which function as carriers of the one or other type of...
US20070138335 Anti-rebound locking device for the deployable fin of a projectile  
The invention relates to a locking device for a deployable surface or fin of a projectile characterized in that it incorporates at least one flexible tongue, one end of which protrudes in the...
US20090008496 Wing-Unfolding Apparatus, Folding Wing Assembly, and Vehicle with Folding Wing Assemblies  
An apparatus for wing unfolding is particularly suited for an airborne vehicle. The apparatus has a base body with a longitudinal axis, a number of moveable flaps, and a number of lateral...
US20120074256 COMPRESSION SPRING WING DEPLOYMENT INITIATOR  
A wing deploy initiator for deploying guidance wings of a rocket or missile, such as the APKWS, provides enhanced wing deploy performance with reduced complexity, cost, and likelihood of failure....
US20110180655 DEVICE FOR SIMULTANEOUS DEPLOYMENT OF THE CONTROL SURFACES OF A PROJECTILE  
A simultaneous deployment device for the control surfaces of a projectile for which each control surface is intended to be pivoted by a motor after its deployment to ensure the piloting, each...
US20130193265 Steering Section for Guided Munition  
A steering section for guided munition comprises a steering body having n control surfaces folded inside or deployed protruding from the external surface. The steering section comprises a locking...
US20120068002 GUIDED MISSILE  
A missile (10) comprising a projectile body (20), a payload (60) contained within the nose portion (30), wings (70) stowed within the mid portion (40), and fins (80) stored within the tail portion...
US20140291441 ROCKET NOZZLE ASSEMBLY  
In one example, a rocket nozzle assembly is disclosed that has stowed and deployed positions, and includes a casing including an outer wall and an inner surface, at least a portion of the inner...
US20120175460 MULTI-STAGE FIN DEPLOYMENT ASSEMBLY  
A multi-stage fin deployment assembly includes a rotary actuator configured to release a first spring-loaded stage that, when deployed, releases a second spring-loaded stage to deploy a set of...

Matches 1 - 10 out of 10