The Aeroassist Flight Experiment (AFE) has several different flight modes associated with its mission. The effect the spacecraft attitude control system (ACS) has on the Reaction Control System (RCS) requirements for all the flight modes is discussed. The ACS requirements and their consequences on the design of the RCS is then discussed in detail. Special problems in the RCS design unique to the AFE mission and the design solutions to these problems are presented.


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    Titel :

    Aeroassist Flight Experiment Reaction Control System preliminary design


    Beteiligte:
    Langford, G. K. (Autor:in) / Price, D. E. (Autor:in) / Gallaher, M. W. (Autor:in)

    Erscheinungsdatum :

    01.07.1990


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Aeroassist Flight Experiment Reaction Control System preliminary design

    LANGFORD, G. / PRICE, D. / GALLAHER, M. | AIAA | 1990


    The Aeroassist Flight Experiment

    Walberg, G. D. / Siemers, P. M., III / Calloway, R. L. et al. | NTRS | 1987


    Aeroassist Flight Experiment (AFE)

    Siemers, Paul M., III | NTRS | 1988


    Aeroassist Flight Experiment (AFE)

    P. M. Siemers | NTIS | 1988


    Radiometer experiment for the aeroassist flight experiment

    DAVY, W. / PARK, C. / ARNOLD, J. et al. | AIAA | 1985