STUDY OF AN ENDOTHERMIC FUEL FOR THE ATLAS ROCKET MOTOR.

Abstract

An analytical and experimental investigation was made of the heat transfer characteristics of TIB (tetraisobutylene) to determine the potential of this fuel as a replacement for RP-1 in an Atlas engine with FLOX (fluorine-liquid oxygen) oxidizer. Under regenerative cooling conditions of surface and fluid temperature, the heat sink from the endothermic dissociation of this fluid could not be realized. Experiments also evaluated the heat transfer characteristics of RP-1 at fluid temperatures over 300 F. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 30, 1965
Accession Number
AD0474712

Entities

People

  • J. D. Seader
  • J. G. Gerstley
  • W. S. Hines

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Cooling
  • Dissociation
  • Engines
  • Fluorine
  • Heat Sinks
  • Heat Transfer
  • Liquid Oxygen
  • Regenerative Cooling
  • Rocket Engines
  • Rockets

Fields of Study

  • Engineering

Readers

  • Business Analytics
  • Combustion and Flow Dynamics.
  • Combustion science or combustion engineering.