Enhanced Ejection Seat Performance with Vectored Thrust Capability.

Abstract

The SAFEST Computer Program and the EASIEST Computer Program were used to predict improved escape performance capabilities resulting from a vectored thrust control system. A parametric study is identified and the results described to quantitatively establish enhanced performance envelope growth of the state-of-the-art ejection seat with an advanced controllable vectored thrust propulsion capability.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1985
Accession Number
ADA161052

Entities

People

  • Edward O. Roberts
  • Lanny A. Jines

Organizations

  • Wright Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Human Systems
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Air Force
  • Air Force Facilities
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Altitude
  • Computer Programs
  • Computers
  • Control Systems
  • Ejection Seats
  • Escape Systems
  • Fighter Aircraft
  • Stabilization Systems
  • Thrust
  • Vehicle Equipment
  • Vehicles

Readers

  • Aerospace Propulsion Engineering.
  • Electrical Engineering
  • Systems Analysis and Design