<--- Back to Details
First PageDocument Content
Transport / Rocket engines / Spacecraft propulsion / Jet engines / Thermodynamics / Thrust vectoring / Space Shuttle Main Engine / Aerospike engine / Expander cycle / Rocket propulsion / Space technology / Aerospace engineering
Date: 2010-01-30 11:35:58
Transport
Rocket engines
Spacecraft propulsion
Jet engines
Thermodynamics
Thrust vectoring
Space Shuttle Main Engine
Aerospike engine
Expander cycle
Rocket propulsion
Space technology
Aerospace engineering

Add to Reading List

Source URL: www.pwrengineering.com

Download Document from Source Website

File Size: 257,24 KB

Share Document on Facebook

Similar Documents

Rocket engines / Transport / Rocket propulsion / Liquid-propellant rocket / LE-5 / Expander cycle / Multistage rocket / RL10 / Spacecraft propulsion / Space technology / Aerospace engineering

DETERMINATION METHOD OF OPTIMUM MAIN DESIGN PARAMETERS OF LOX-LH2 EXPANDER-CYCLE LRE

DocID: akTz - View Document

Rocket propulsion / Transport / Spacecraft propulsion / Expander cycle / LE-5 / Liquid-propellant rocket / Staged combustion cycle / Space Shuttle Main Engine / F-1 / Rocket engines / Rocketry / Space technology

Sample of Paper for Journal of the Japan Society for

DocID: 4Svp - View Document

Aerospace engineering / Spacecraft propulsion / Rocket propulsion / North American Aviation / Thermodynamics / RL10 / Expander cycle / Space Shuttle Main Engine / RD-0146 / Rocket engines / Rocketry / Space technology

Program Status of the Pratt & Whitney RL60 Engine J.R. Bullock, M. Popp, J.R. Santiago Pratt & Whitney Space Propulsion

DocID: 4MJX - View Document

Rocket propulsion / Transport / Jet engines / Spacecraft propulsion / Aerospace engineering / Space Shuttle Main Engine / Liquid-propellant rocket / RD-270 / Expander cycle / Rocket engines / Space technology / Rocketry

IAC-12-C4.1.11 PRELIMINARY DESIGN STUDY OF STAGED COMBUSTION CYCLE ROCKET ENGINE FOR SPACELINER HIGH-SPEED PASSENGER TRANSPORTATION CONCEPT

DocID: 43EA - View Document

Spacecraft propulsion / Transport / Rocket propulsion / Chemical Automatics Design Bureau / Liquid-propellant rocket / J-2 / Expander cycle / RL10 / Space Shuttle Main Engine / Rocket engines / Space technology / Rocketry

RD-0146: The First LOX-LH2 Expander Cycle Liquid Rocket Engine in Russia

DocID: 41YK - View Document