Liquid Propellants Symposium, 27-28 March 1957

Abstract

Contents include (but not limited to): An Evaluation of Liquid Ozone-Oxygen Mixtures as Rocket Oxidizers (Layton, Glassman, Garvin); Hydrogen Peroxide Propellants (Kubica, Keefe); Heat Transfer Properties of Anhydrous Ammonia (Reinhardt, Potter, Moore); Performance of Perchloryl Fluoride (Mickle, Berman, Gantz); The Tangential Mode of Combustion Instability (Pickford, Ellis); A Non-Coking Ethylene Oxide Reactor (Smith); High Energy Fuels in Air Breathing Engines (DeZubay, King); and others.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1957
Accession Number
AD0128783

Entities

Organizations

  • United States Assistant Secretary of Defense

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Ground and Sea Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Chemical Elements
  • Chemical Synthesis
  • Chemistry
  • Heat Energy
  • Heat Transfer
  • Ignition Lag
  • Material Degradation Processes
  • Materials Laboratories
  • Materials Processing
  • Materials Science
  • Organic Chemistry
  • Rocket Oxidizers
  • Thermodynamics

Readers

  • Combustion science or combustion engineering.
  • Military History
  • Rocket Propulsion.