Secondary Injection Actuated Gimbaled Motor.

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.

Document Details

Document Type
Technical Report
Publication Date
Feb 07, 1974
Accession Number
ADD000611

Entities

People

  • W. Jame Stone

Organizations

  • United States Department of the Navy

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Airborne
  • Aircrafts
  • Engines
  • Exhaust Plumes
  • Fluids
  • Parachutes
  • Patent Applications
  • Patents
  • Plumes
  • Rocket Engines
  • Rockets
  • Secondary Injection

Readers

  • Combustion and Flow Dynamics.
  • Explosive Engineering.
  • Robotics and Automation.