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

Abstract

Contents: I. Coated Metallic Thrust Chambers; II. Expandable Nozzles; III. Combustion Instability Scaling Concepts; IV. Ablative Thrust Chambers.

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Document Details

Document Type
Technical Report
Publication Date
Nov 15, 1963
Accession Number
AD0423407

Entities

Organizations

  • Aerojet Rocketdyne Holdings

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Chambers
  • Combustion
  • Combustion Chambers
  • Contracts
  • Engineering
  • Engines
  • Fabrication
  • Film Cooling
  • Heat Transfer
  • Materials
  • Rocket Engines
  • Rockets
  • Thrust Chambers
  • Variable Area Nozzles
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Control Systems Engineering.
  • Software Engineering