Experimental performance of the mixed-oxides-of-nitrogen-ammonia propellant combination in a 1000-pound-thrust rocket engine Metadata

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Title

  • Main Title Experimental performance of the mixed-oxides-of-nitrogen-ammonia propellant combination in a 1000-pound-thrust rocket engine
  • Series Title NACA Research Memorandums

Creator

  • Author: Tomazic, William A.
    Creator Type: Personal
  • Author: Kinney, George R.
    Creator Type: Personal

Contributor

  • Originator: Lewis Flight Propulsion Laboratory
    Contributor Type: Organization
    Contributor Info: National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab

Date

  • Creation: 1955-03-28

Language

  • English

Description

  • Content Description: An investigation of the performance of the mixed-oxides-of-nitrogen-ammonia propellant combination over a range of conditions with several injectors. Results regarding specific impulse, characteristic velocity, and thrust coefficient as functions of oxidant-fuel weight ratio are provided.
  • Physical Description: 30 p. : ill.

Subject

  • Keyword: aircraft fuel
  • Keyword: fuel injectors
  • Keyword: aircraft propellants

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: 93R17901
  • URL: http://hdl.handle.net/2060/19930088611
  • Report No.: NACA-RM-E55A07
  • Center for AeroSpace Information Number: 19930088611
  • Archival Resource Key: ark:/67531/metadc61181