Engine data and information are presented to perform system studies on cargo orbit-transfer vehicles which would deliver large space structures to geosynchronous equatorial orbit. Low-thrust engine performance, weight, and envelope parametric data were established, preliminary design information was generated, and technologies for liquid rocket engines were identified. Two major engine design drivers were considered in the study: cooling and engine cycle options. Both film-cooled and regeneratively cooled engines were evaluated. The propellant combinations studied were hydrogen/oxygen, methane/oxygen, and kerosene/oxygen.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Low-Thrust Chemical Rocket Engine Study


    Contributors:

    Publication date :

    1981


    Size :

    152 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Low-thrust chemical rocket engine study

    Mellish, J. A. | NTRS | 1981



    Toward variable-thrust liquid-rocket engine

    Welton, D.E. / Bensky, S.M. / Hiland, J.R. | Engineering Index Backfile | 1963


    Validation of Stream Thrust Probes for Rocket Engine Thrust Measurement

    Hiers, Robert / MacKinnon, H. / Whitney, R. et al. | AIAA | 2003


    Low thrust chemical rocket technology

    Schneider, Steven J. | NTRS | 1992