Penalties Incurred in Using Rocket Motors over a Wide Temperature Range

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1951
Accession Number
ADA474137

Entities

People

  • M. Goyer

Organizations

  • Royal Aircraft Establishment

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Burning Rate
  • Climate Change
  • Combustion
  • Combustion Chambers
  • Composite Propellants
  • Double Base Propellants
  • Guided Missiles
  • Guided Weapons
  • Ignition Lag
  • Liquid Propellants
  • Liquid Rocket Oxidizers
  • Material Degradation Processes
  • Materials Laboratories
  • Plastic Explosives
  • Rocket Engines
  • Rocket Oxidizers
  • Solid Propellants