MANEUVERING SATELLITE PROPULSION SYSTEM DEMONSTRATION. PART 3

Abstract

This document presents the exploratory development work accomplished in the design, fabrication and testing of advanced rocket engine components for a high-energy-propellant, space maneuvering vehicle. The exploratory development effort consisted of a series of critical experiments to determine operational capabilities of high temperature material and coating in fluorine rich and HF environments, the feasibility of a wide range throttling concept utilizing mixed phase propellants, and the feasibility of an advanced thrust chamber cooling concept.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1965
Accession Number
AD0368603

Entities

People

  • J. Germano
  • M. Chazen
  • W. Pearson

Organizations

  • Bell Aircraft Corporation

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Artificial Satellites
  • Assembly
  • Chemistry
  • Composite Materials
  • Crystal Structure
  • Fabrication
  • Generators
  • Heat Energy
  • Heat Transfer
  • Material Degradation Processes
  • Materials
  • Materials Laboratories
  • Materials Processing
  • Materials Science
  • Materials Testing
  • Propulsion Systems
  • Transition Temperature

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.
  • Software Engineering

Technology Areas

  • Space
  • Space - Hall-Effect Thruster