First Page | Document Content | |
---|---|---|
Date: 2003-07-14 10:14:48Rocketry Transport Spacecraft propulsion LE-5 Expander cycle Rocket engine Liquid-propellant rocket Cryogenic rocket engine Regenerative cooling Space technology Rocket engines Rocket propulsion | Add to Reading ListSource URL: www.la.dlr.deDownload Document from Source WebsiteFile Size: 1,72 MBShare Document on Facebook |
DETERMINATION METHOD OF OPTIMUM MAIN DESIGN PARAMETERS OF LOX-LH2 EXPANDER-CYCLE LREDocID: akTz - View Document | |
Sample of Paper for Journal of the Japan Society forDocID: 4Svp - View Document | |
Program Status of the Pratt & Whitney RL60 Engine J.R. Bullock, M. Popp, J.R. Santiago Pratt & Whitney Space PropulsionDocID: 4MJX - View Document | |
IAC-12-C4.1.11 PRELIMINARY DESIGN STUDY OF STAGED COMBUSTION CYCLE ROCKET ENGINE FOR SPACELINER HIGH-SPEED PASSENGER TRANSPORTATION CONCEPTDocID: 43EA - View Document | |
RD-0146: The First LOX-LH2 Expander Cycle Liquid Rocket Engine in RussiaDocID: 41YK - View Document |