Star Tracker LEO

    • Star Tracker LEO

    Purpose:
    Star based satellite attitude determination
    Year of release: 2019
    Guaranteed service life (years): 5
    Estimated production / delivery time (months): 6
    Flight qualification of the product: No
    Brief history of flight qualification:
    Prototype flight experience over 7 years
    Possibility to adapt the product to customer requirements: Yes
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    Parameter Value
    Random error (1-sigma) across boresight at 22 Hz 1,5 arcsec
    Random error (1-sigma) boresight at 22 Hz 10 arcsec
    Random error (1-sigma) across boresight at 10 Hz 1 arcsec
    Random error (1-sigma) boresight at 10 Hz 7 arcsec
    Mass (including 30 grad baffle) 0,5 kg
    Dimensions (including 30 grad baffle) 149 х100 х137 mm
    Power consumption 5 W
    Sun exclusion angle 30 grad
    Power 10…32 V
    Temperature range minus 40… plus 50

    Description

    Autonomous Star Tracker

    Remark

    Designed for LEO up to 1200

    Legal information
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