Theoretical performance of liquid ammonia and liquid fluorine as a rocket propellant Metadata

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Title

  • Main Title Theoretical performance of liquid ammonia and liquid fluorine as a rocket propellant
  • Series Title NACA Research Memorandums

Creator

  • Author: Gordon, Sanford
    Creator Type: Personal
  • Author: Huff, Vearl N.
    Creator Type: Personal

Contributor

  • Originator: Lewis Flight Propulsion Laboratory
    Contributor Type: Organization
    Contributor Info: NASA Lewis Research Center

Date

  • Creation: 1953-07-03

Language

  • English

Description

  • Content Description: From Summary: "Theoretical values of performance parameters for liquid ammonia and liquid fluorine as a rocket propellant were calculated on the assumption of equilibrium composition during the expansion process for a wide range of fuel-oxidant and expansion ratios. The parameters included were specific impulse, combustion-chamber temperature, nozzle-exit temperature, equilibrium composition, mean molecular weight, characteristic velocity, coefficient of thrust, ratio of nozzle-exit area to throat area, specific heat at constant pressure, coefficient of viscosity, and coefficient of thermal conductivity."

Subject

  • Keyword: aircraft fuels
  • Keyword: ammonia
  • Keyword: fluorine
  • Keyword: chemical properties

Collection

  • Name: National Advisory Committee for Aeronautics Collection
    Code: NACA
  • Name: Technical Report Archive and Image Library
    Code: TRAIL

Institution

  • Name: UNT Libraries Government Documents Department
    Code: UNTGD

Rights

  • Rights Access: public
  • Rights License: pd
  • Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available

Resource Type

  • Report

Format

  • Text

Identifier

  • Accession or Local Control No: 65N87349
  • URL: http://hdl.handle.net/2060/19650074946
  • Report No.: NACA-RM-E53A26
  • Center for AeroSpace Information Number: 19650074946
  • Archival Resource Key: ark:/67531/metadc53029