Accession Number : ADD000611
Title : Secondary Injection Actuated Gimbaled Motor.
Descriptive Note : Patent Application,
Corporate Author : DEPARTMENT OF THE NAVY WASHINGTON D C
Personal Author(s) : Stone,W Jame
Report Date : 07 Feb 1974
Pagination or Media Count : 7
Abstract : The patent application relates to a device whereby the attitude of an airborne load is controlled by injecting fluid into the exhaust plume of a rocket motor which is attached to the load by gimbals and drives the load. In particular, it relates to apparatus and a method for controlling the attitude of a seat and a crew member sitting in the seat just after the seat and crew member have been ejected from an aircraft and before the crew member's parachute opens.
Descriptors : *Solid propellant rocket engines, *Attitude control systems, *Secondary injection, Patents, Gimbals, Fluid control, Ejection seats
Subject Categories : Aircraft
Solid Propellant Rocket Engines
Escape, Rescue and Survival
Distribution Statement : APPROVED FOR PUBLIC RELEASE