PROPELLANT ACTUATED DEVICES

Abstract

Contents: High Temperature Propellants for Crew Escape System Rockets; Feasibility of a Hybrid Rocket for Crew Escape Capsule Application; Propellant Actuated Devices in Space Environment; Close Tolerance Delay; Ancillary Components for Escape Systems; Mild Detonating Fuse (MDF); Components for Electrically Initiated Escape Systems; Co-Axial Catapult; Time Delay Mechanism; Dyna-Soar Technical Assistance; XM18 Gas Generator; Characteristics of Dynamic Seals, Sealing Materials, and Sealing Techniques for PAD; Improved Propellants and Primers for PAD Applications; Investigation of Recently Developed Materials and Manufacturing Techniques for Application to PAD; Improvement of PAD to Eliminate Toxic Propellant Gases (2 Reports); Medium Performance Miniature Initiator; Development of Ballistic Reel; Gun Launched Rocket; Rocket Altitude Sensing and Thrust Direction Control; Development of Twenty-Man Life Raft Inflator; Heavyduty Pyrotechnic Delay Reefing Line Cutter; and Bomb Ejector Cartridge for MAU-12/A Bomb Rack.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1963
Accession Number
AD0439662

Entities

Organizations

  • Frankford Arsenal

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Chemistry
  • Engineers
  • Escape Systems
  • Fabrication
  • High Temperature
  • Manufacturing
  • Materials Laboratories
  • Materials Processing
  • Materials Science
  • Military Aircraft
  • Munitions
  • Nitrogen Oxides
  • Rocket Engines
  • Rocket Oxidizers
  • Systems Engineering
  • Test And Evaluation

Fields of Study

  • Physics

Readers

  • Electrical Engineering
  • Explosive Engineering.
  • Materials Science

Technology Areas

  • Space
  • Space - Hall-Effect Thruster
  • Space - Spacecraft Maneuvers