The science experiments for the Aeroassist Flight Experiment (AFE) will be greatly enhanced by taking measurements with no Reaction Control System (RCS) contamination just before perigee. Methods of modifying the AFE guidance to accomplish this are discussed. Several methods that could give up to 30 seconds of quiet time were investigated and the results of these guidance modifications shown. A 20 second quiet time is definitely possible and a 30 second quiet time may be possible if the guidance can be inactive past perigee. Some of the most significant being the criterion for determining if the mission is threatened. A limited follow-on test program is outlined.


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    Titel :

    Aeroassist Flight Experiment Guidance Quiet Time


    Beteiligte:
    S. A. Striepe (Autor:in) / W. T. Suit (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    78 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Striepe, Scott A. / Suit, William T. | NTRS | 1988


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    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