THROTTLING AND SCALING STUDY FOR ADVANCED STORABLE ENGINE. PART 2. APPENDIX 1. ARES SIZE SCALING DATA
Final rept. 10 Jul-10 Oct 1967
AEROJET-GENERAL CORP SACRAMENTO CA LIQUID ROCKET DIV
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The Advanced Rocket Engine Storable ARES, described in this appendix, is a throttlable-restartable advanced rocket engine using storable N2O4AeroZINE 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.
- Liquid Propellant Rocket Engines
- Liquid Rocket Propellants