PRODUCT ENGINEERING PROGRAM. COATED METALLIC THRUST CHAMBERS EXPANDABLE NOZZLES COMBUSTION INSTABILITY SCALING CONCEPTS ABLATIVE THRUST CHAMBERS. WEAPON SYSTEM 107A-2

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Document Details

Document Type
Technical Report
Publication Date
Oct 15, 1963
Accession Number
AD0421614

Entities

Organizations

  • Aerojet Rocketdyne Holdings

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Combustion
  • Combustion Chambers
  • Engineering
  • Exhaust Nozzles
  • Fabrication
  • Film Cooling
  • Flow Rate
  • Heat Transfer
  • Materials
  • Materials Processing
  • Materials Science
  • Measurement
  • Physics Laboratories
  • Rocket Engines
  • Rocket Propulsion
  • Thrust Chambers