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.
Secondary Injection Actuated Gimbaled Motor
1974
7 pages
Report
Keine Angabe
Englisch