EXPERIMENTAL PERFORMANCE AND HEAT TRANSFER CHARACTERISTICS OF 90 PERCENT HYDROGEN PEROXIDE AND JET ENGINE FUEL, JP-5, ROCKET PROPELLANTS AT 500 PSIA, 750 PSIA AND 1000 PSIA COMBUSTION PRESSURE

Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1957
Accession Number
AD0301253

Entities

People

  • D.l. Emmons
  • P.m. Diamond

Organizations

  • Purdue University

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Chemical Reactions
  • Combustion
  • Energetic Materials
  • Engines
  • Exothermic Reactions
  • Fuels
  • Heat Transfer
  • Hydrogen
  • Ignition
  • Jet Engine Fuels
  • Jet Engines
  • Materials
  • Propellants
  • Rocket Oxidizers
  • Rocket Propellants