Rocket Engines - Liquid Propellant. Volume 1 - Small Engines

Abstract

This document contains information on rocket engines using propellants stored as liquids or gases. Volume 1 contains information on engines used for reaction control systems and low velocity increment propulsion systems. Cold (ambient) gas, heated gas, monopropellant and bipropellant engines are considered. Estimates are made of performance, size and power requirements. Operating principles, hardware details and systems consideration are discussed.

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Document Details

Document Type
Technical Report
Publication Date
Oct 30, 1968
Accession Number
AD0843667

Entities

People

  • H. R. Bader Jr.

Organizations

  • Boeing

Tags

Communities of Interest

  • Energy and Power Technologies
  • Ground and Sea Platforms
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Chemical Reaction Properties
  • Chemical Reactions
  • Chemistry
  • Combustion
  • Control Systems
  • Heat Capacity
  • Ignition Lag
  • Materials Laboratories
  • Materials Science
  • Nitrogen Oxides
  • Propellants
  • Propulsion Systems
  • Rocket Engines
  • Rocket Oxidizers
  • Spacecraft
  • Specific Heat
  • Thrusters

Fields of Study

  • Physics

Readers

  • Aerospace Propulsion Engineering.
  • Combustion and Flow Dynamics.
  • Software Engineering