WEAPON SYSTEM 107A-2. PRODUCT ENGINEERING PROGRAM

Abstract

Contents: Coated metajlic thrust chambers; Ex pandable nozzles; Combustion instability scaling concepts; and Ablative thrust chambers.

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Document Details

Document Type
Technical Report
Publication Date
Jul 31, 1963
Accession Number
AD0414585

Entities

Organizations

  • Aerojet Rocketdyne Holdings

Tags

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Combustion
  • Combustion Chambers
  • Engineering
  • Fabrication
  • Film Cooling
  • Heat Flux
  • Heat Transfer
  • Jet Propulsion
  • Materials
  • Propellants
  • Rocket Engines
  • Rockets
  • Test Facilities
  • Thrust Chambers
  • Wind Tunnels

Fields of Study

  • Physics