This paper explores some of the many considerations which enter into the choice of a specific spacecraft propulsion system for a particular application. The environment and its influence on propulsion requirements are discussed in general terms, characteristics of several propellant combinations are presented and an example of a typical ambitious mission is used.A general conclusion is that the state of the art of spacecraft propulsion technology must advance on a broad front in the time period prior to project definition in order to provide the technological options which allow significant optimization of the complete project propulsion system.


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    Titel :

    Requirements for Space Propulsion Systems


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Space Technology Conference ; 1968



    Erscheinungsdatum :

    1968-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Requirements for Space Propulsion Systems

    R. H. Rollins / W. W. Wilcox | NTIS | 1968


    Requirements for space propulsion systems.

    Rollins, R. H., II / Wilcox, W. W. | NTRS | 1968


    Requirements for Space Propulsion Systems

    Rollins, R. H., II / Wilcox, W. W. | NTRS | 1968


    Requirements for space propulsion systems

    Wilcox, W.W. / Rollins II, R.H. | Engineering Index Backfile | 1968


    Large space systems auxiliary propulsion requirements

    Maloy, J. E. / Smith, W. W. | NTRS | 1983