F-Sat is a standard spacecraft bus which will support future LMSC programs, both commercial and government. The F-Sat bus has been designed with the adaptability to satisfy any applications with medium-weight payloads. This paper discusses F-Sat's design and a recently completed test which demonstrated the integration of flight electronics with attitude determination and control system sensors and actuators. With the successful completion of this demonstration. F-Sat has taken one more step toward realizing the goal of low cost access to space.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Development status of FSAT: a standard spacecraft bus


    Beteiligte:
    Beals, Gary A. (Autor:in) / Gerbasi, Marty (Autor:in) / Rust, William M. (Autor:in)

    Kongress:

    Acquisition, Tracking, and Pointing VIII ; 1994 ; Orlando,FL,United States


    Erschienen in:

    Proc. SPIE ; 2221 ; 70


    Erscheinungsdatum :

    05.07.1994





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Development status of FSAT: a standard spacecraft bus [2221-08]

    Beals, G. A. / Gerbasi, M. / Rust, W. et al. | British Library Conference Proceedings | 1994


    Development Status of Spacecraft

    C. Ishida | NTIS | 1990


    Spacecraft charging standard

    Holman, A. B. / Bunn, M. H. | NTRS | 1979


    Development status of Multi-utility Spacecraft Cha...

    Hatta, Shinji / Muranaka, Takanobu / Hosoda, Satoshi et al. | AIAA | 2005


    CloudSat spacecraft status

    Vane, Deborah | NTRS | 2018