Synonyme wurden verwendet für: engine
Suche ohne Synonyme: keywords:(J- 2 rocket engine)

1–20 von 63 Ergebnissen
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    System Engineering and Technical Challenges Overcome in the J-2X Rocket Engine Development Project

    R. O. Ballard | NTIS | 2012
    Schlagwörter: Rocket Engines & Motors , J-2 engine , Rocket engines , Engine design

    Altitude Testing of Large Liquid Propellant Engines

    B. Maynard / N. Raines | NTIS | 2008
    Schlagwörter: Rocket Propellants , Rocket Engines & Motors , J-2 engine , Liquid propellant rocket engines , Engine design , Liquid rocket propellants

    Experimental study on the working performance of powdered magnesium and liquid carbon dioxide bipropellant rocket engine for Mars missions

    Hu, Jiaming / Hu, Chunbo / Che, Yanhong et al. | Elsevier | 2021
    Schlagwörter: Liquid CO2 , Powder rocket engine

    NASA/JAXA Exploration Collaboration F2F

    S Creech | NTIS | 2013
    Schlagwörter: Rocket Engines & Motors , J-2 engine , Engine tests , Booster rocket engines

    The s-ii stage of saturn v launch vehicle.

    Wickham, P. L. | NTRS | 1964
    Schlagwörter: J-2 ROCKET ENGINE , SATURN S-2 STAGE , MULTISTAGE ROCKET

    Materials in NASA's Space Launch System: The Stuff Dreams are Made of

    T. A. May | NTIS | 2012
    Schlagwörter: Multistage rocket vehicles , J-2 engine , Booster rocket engines

    Design specifications of H2O2/kerosene bipropellant rocket system for space missions

    Moon, Yongjun / Park, Chul / Jo, Sungkwon et al. | Elsevier | 2014
    Schlagwörter: H2O2/kerosene bipropellant rocket system , Apogee kick motor

    Combustion performance and scale effect from N2O/HTPB hybrid rocket motor simulations

    Shan, Fanli / Hou, Lingyun / Piao, Ying | Elsevier | 2012
    Schlagwörter: N2O/HTPB hybrid rocket motor

    Pressure-drop characteristics of CO2 boiling flow in the regenerative-cooling channel of an Mg/CO2 powder rocket engine for Mars missions

    Wei, Ronggang / Hu, Chunbo / Yang, Jiangang et al. | Elsevier | 2022
    Schlagwörter: Powder rocket engine , CO2

    Foundation for Heavy Lift: Early Developments in the Ares V Cargo Launch Vehicle

    J. P. Sumrall / J. C. McArthur | NTIS | 2007
    Schlagwörter: Rocket launching , J-2 engine , Booster rocket engines

    Electro-pneumatic actuation system Interim technical report

    Trautner, M. C. | NTRS | 1966
    Schlagwörter: J-2 ROCKET ENGINE

    Heat-transfer characteristics of CO 2 boiling flow in the regenerative cooling channel of an Mg/CO 2 powder rocket engine for Mars missions

    Wei, Ronggang / Hu, Chunbo / Wu, Fuzhen et al. | Elsevier | 2021
    Schlagwörter: Powder rocket engine , CO2

    Development of the J-2X Engine for the Ares I Crew Launch Vehicle and the Ares V Cargo Launch Vehicle: Building on the Apollo Program for Lunar Return Missions

    W. I. Greene | NTIS | 2007
    Schlagwörter: Rocket Engines & Motors , J-2 engine , Engine design , Engine tests

    J-2 Engine as-502 ( Apollo 6) Flight Report S-2 and S-4 B Stages. Volume 2 - S-2 Stage Failure Analysis

    NTIS | 1968
    Schlagwörter: Rocket Engines & Motors , Engine failure , J- 2 engine , Engine monitoring instruments , Rocket nozzles , Saturn s- 2 stage

    REIMR - A Process for Utilizing Liquid Rocket Propulsion-Oriented 'Lessons Learned' to Mitigate Development Risk in Nuclear Thermal Propulsion

    R. I. O. Ballard | NTIS | 2006
    Schlagwörter: Liquid propellant rocket engines , Rocket engines , J-2 engine

    Dynamic Mechanical Analysis (DMA) to Help Characterize Vespel SP-211 Polyimide Material for Use as a 750 F Valve Seal on the Ares I Upper Stage J-2X Engine

    D Wingard | NTIS | 2013
    Schlagwörter: Rocket Engines & Motors , J-2 engine , Upper stage rocket engines

    Testing for the J-2X Upper Stage Engine

    J. C. Buzzell | NTIS | 2010
    Schlagwörter: J-2 engine , Engine tests , Rocket thrust

    Ares V: Game Changer for National Security Launch

    P. Sumrall / B. Morris | NTIS | 2009
    Schlagwörter: Rocket engines , J-2 engine , Solid propellant rocket engines

    Development of the subliming solid control rocket, phase II

    NTRS | 1967
    Schlagwörter: CONTROL ROCKET , ROCKET NOZZLE , OV2 /ORBITING VEHICLE-2/ , SOLID PROPELLANT ROCKET ENGINE