ADVANCED CRYOGENIC ROCKET ENGINE PROGRAM, AEROSPIKE NOZZLE CONCEPT

Abstract

Program status and technical results obtained at the end of the second 3 months are described for the Advanced Development Program, Aerospike. This program includes analysis and preliminary design of an advanced rocket engine using an aerospike nozzle. It further includes analysis, test hardware design, and test evaluation of thrust chamber performance and thrust chamber durability.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1966
Accession Number
AD0376293

Entities

People

  • F. B. Lary

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Air Force
  • Boundary Layer
  • Closed Loop Systems
  • Combustion Chambers
  • Control Systems
  • Fabrication
  • Heat Transfer
  • Igniters
  • Manufacturing
  • Materials
  • Mechanical Properties
  • Mechanical Working
  • Mechanics
  • Test And Evaluation
  • Test Facilities
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Combustion and Flow Dynamics.
  • Technical Research and Report Writing.