TITAN II. DYNA SOAR

Abstract

The use of storable, high energy and hypergolic pr pellants, Unsymmetrical Dimethyl Hydrazine (UDMH)/Hydrazine and Nitrogen Tetroxide (N2O4), in Titan II and Titan III is an advancement in weapon and space systems. However, the intermixing reaction and toxicological properties of these propellants introduced a problem in the design of the destruct system for the booster. Tests were conducted to develop and verify a booster destruct system for use with these propellants.

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Document Details

Document Type
Technical Report
Publication Date
Mar 15, 1962
Accession Number
AD0274351

Entities

People

  • E. Larsh
  • H. Huntyer

Organizations

  • Glenn L. Martin Company

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Blast
  • Cameras
  • Contracts
  • Energy
  • Explosions
  • Explosives
  • Fuel Tanks
  • Ground Level
  • High Energy
  • Instrumentation
  • Intercontinental Ballistic Missiles
  • Pressure Transducers
  • Rocket Oxidizers
  • Space Systems
  • Strain Gages
  • Transducers

Readers

  • Rocket Propulsion.
  • Systems Analysis and Design

Technology Areas

  • Space
  • Space - Hall-Effect Thruster