CANYVAL-X is a technology demonstration CubeSat mission with a primary objective of validating technologies that allow two spacecraft to fly in formation along an inertial line-of-sight (i.e., align two spacecraft to an inertial source). Demonstration of precision dual-spacecraft alignment achieving fine angular precision enables a variety of cutting-edge heliophysics and astrophysics science.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Canyval-x: Cubesat Astronomy by NASA and Yonsei Using Virtual Telescope Alignment Experiment


    Beteiligte:
    N. Shah (Autor:in)

    Erscheinungsdatum :

    2016


    Format / Umfang :

    2 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    NASA Cubesat/Smallsat Reference Model

    Nancy Lindsey / Lionel- Nobel Sindjui / Mahdi Alimardani | NTRS


    Review of NASA Ames CubeSat Program

    R. Hunter / D. J. Korsmeyer | NTIS | 2015


    NASA Cubesat and Microsat Cost Model

    Johnson, James K. / Lumnah, Alex / Hooke, Melissa et al. | NTRS | 2020