THROTTLING AND SCALING STUDY FOR ADVANCED STORABLE ENGINE. PART 2. APPENDIX 1. ARES SIZE SCALING DATA

Abstract

The Advanced Rocket Engine Storable (ARES), described in this appendix, is a throttlable-restartable advanced rocket engine using storable N2O4/AeroZINE 50 propellants. Parametric performance, size, weight, and cost scaling data for throttlable and restartable ARES liquid-propellant rocket engines over a range of engine sizes with rated thrust values from 25,000 to 500,000 lbf are presented in this report.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1968
Accession Number
AD0387058

Entities

People

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

Organizations

  • Aerojet Rocketdyne Holdings

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Chambers
  • Combustors
  • Engines
  • Government Procurement
  • Governments
  • Law
  • Liquid Propellants
  • National Security
  • Propellants
  • Pumps
  • Rocket Engines
  • Rocket Propulsion
  • Rockets
  • Specific Impulse
  • Thrust Chambers
  • United States

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Rocket Propulsion.