Development and Demonstration of Ablative Thrust Chamber Assemblies Using LF2/N2H4 Blend Propellants

Abstract

The exploratory development effort included the design, fabrication, and testing of injectors, ablative thrust chambers, and a radiation-cooled- divergent nozzle extension.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1969
Accession Number
AD0395844

Entities

People

  • Harold V. Kiser
  • Robert C. Schindler

Organizations

  • Aerojet Rocketdyne Holdings

Tags

Communities of Interest

  • Biomedical
  • Energy and Power Technologies
  • Human Systems
  • Sensors
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Chemical Synthesis
  • Chemistry
  • Fabrication
  • Graphitic Materials
  • Heat Transfer
  • Material Degradation Processes
  • Materials Laboratories
  • Materials Processing
  • Materials Science
  • Materials Testing
  • Mechanical Working
  • Mechanics
  • Resonant Frequency
  • Rocket Engines
  • Test And Evaluation
  • Thermodynamics

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Software Engineering