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Accession Number:
AD0387058
Title:
THROTTLING AND SCALING STUDY FOR ADVANCED STORABLE ENGINE. PART 2. APPENDIX 1. ARES SIZE SCALING DATA
Corporate Author:
AEROJET-GENERAL CORP SACRAMENTO CA LIQUID ROCKET DIV
Report Date:
1968-01-01
Abstract:
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.
Descriptive Note:
Final rept. 10 Jul-10 Oct 1967
Supplementary Note:
See also Part 1, AD387057.
Pages:
0024
Distribution Statement:
Approved for public release; distribution is unlimited.
Contract Number:
F04611-68-C-0008
File Size:
1.21MB
