Accession Number:

AD0387058

Title:

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

Descriptive Note:

Final rept. 10 Jul-10 Oct 1967

Corporate Author:

AEROJET-GENERAL CORP SACRAMENTO CA LIQUID ROCKET DIV

Personal Author(s):

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

Report Date:

1968-01-01

Pagination or Media Count:

24.0

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.

Descriptors:

• *LIQUID PROPELLANT ROCKET ENGINES
• STORABLE ROCKET PROPELLANTS
• COSTS
• WEIGHT
• STARTING
• THRUST
• LIQUID ROCKET PROPELLANTS
• SPECIFIC IMPULSE
• ENGINE STARTERS
• MOMENT OF INERTIA
• GIMBALS
• NOZZLE AREA RATIO
• BELL NOZZLES
• THROTTLING
• PERFORMANCE(ENGINEERING)

Subject Categories:

• Liquid Propellant Rocket Engines
• Liquid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE