Study and Design of an Ejection System for VTOL Aircraft, Part 2, Volume 1, Escape Seat System Concept Analysis

Abstract

An ejection seat escape system is described for hypothetical two-place fighter-attach VTOL aircraft.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1970
Accession Number
AD0871324

Entities

People

  • E. O. Jr Cartwright
  • I. L. Clinkenbeard

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Altitude
  • Axial Loads
  • Dynamic Response
  • Dynamics
  • Ejection Seats
  • Escape Systems
  • Export Controls
  • Exports
  • Failure Mode And Effect Analysis
  • Governments
  • Parachutes
  • Radar Altimeters
  • Reliability
  • Rocket Engines
  • Trajectories

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Engineering