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![]() Date: 2010-10-04 05:35:25Space technology Rocketry LE-7 LE-5 H-IIB Expander cycle H-II Japanese space program Spaceflight Rocket engines | Add to Reading List |
![]() | 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 |