PROTOTYPE PROPELLANT-TESTING SYSTEM. PHASES 1 AND 2 - FEASIBILITY STUDY AND PRELIMINARY DESIGN

Abstract

The feasibility of constructing a test system for studying dynamic effects in liquid-propellant streams was examined and a prototype system was designed that is acceptable for use with storable, corrosive, or cryogenic fuels and oxidizers. Recommendations are made for on-stream analyzers suitable for the monitoring of a wide range of physical and bsequent tests.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1963
Accession Number
AD0297040

Entities

People

  • H. C. Edgington
  • R. C. Adrian

Organizations

  • Aerojet Rocketdyne Holdings

Tags

Communities of Interest

  • Advanced Electronics
  • Biomedical
  • Energy and Power Technologies
  • Ground and Sea Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Cameras
  • Chemical Synthesis
  • Chemistry
  • Liquid Propellants
  • Mass Spectrometry
  • Material Degradation Processes
  • Materials Laboratories
  • Materials Processing
  • Materials Science
  • Measurement
  • Measuring Instruments
  • Monitors
  • Rocket Oxidizers
  • Spectrometry
  • Spectroscopy
  • Telemetry Equipment

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Rocket Propulsion.
  • Software Engineering