THROTTLING AND SCALING STUDY FOR ADVANCED STORABLE ENGINE. PART 1

Abstract

This report documents the technical accomplishments of the ARES (advanced Rocket Engine Storable) Throttling and Scaling Study Program. Included also in this report is the sponsored design of a throttlable- restartable 100K ARES engine which was used as the baseline engine for this design study. Throttlable, restartable ARES (Advanced Rocket Engine Storable) engine designs are presented at 25,000, 100,000, and 500,000 lb rated thrust levels. On the basis of these designs, engine thrust scaling parametric data are presented over a thrust range of 25,000 to 500,000 lb with nozzle expansion ratios of 50:1 and 150:1.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1968
Accession Number
AD0387057

Entities

People

  • A. W. Nelson
  • H. L. Bishop
  • J. A. Gibb
  • R. E. Duckering
  • Stanley R. Andrus

Organizations

  • Aerojet Rocketdyne Holdings

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Classification
  • Combustion
  • Computers
  • Contracts
  • Control Systems
  • Differential Equations
  • Film Cooling
  • Flow
  • Fuel Pumps
  • Fuel Tanks
  • High Pressure
  • Ignition
  • Pressurization
  • Propellant Tanks
  • Propellants
  • Rocket Engines

Fields of Study

  • Physics

Readers

  • Internal Combustion Engine (ICE) Technology.
  • Technical Research and Report Writing.