Gyroscope Sensor for Measuring Angular Velocity Vector Projections-4

    • Gyroscope Sensor for Measuring Angular Velocity Vector Projections-4

    Purpose:
    Measurement of angular increments (rate integral) on sensitive axes of four measurement channels and transmission of that information to the object’s control system.
    Year of release: 2019
    Guaranteed service life (years): 17
    Flight qualification of the product: No
    Brief history of flight qualification:
    The instrument is being developed for future spacecrafts.
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    Parameter Value
    Measurement range ±100°/s
    Random component of the zero signal in a particular switch-on lasting 24 hours with an averaging time of 100 s not more than 10-3 °/h
    Working conditions Outer space
    Weight 13 kg

    Description

    Redundant free form gyroscopic angular velocity vector meter for spacecraft orientation and stabilization control system. An unsealed two-block construction including an electronic device unit with four independent channels consisting of electronic and optoel
    ... Redundant free form gyroscopic angular velocity vector meter for spacecraft orientation and stabilization control system.
    An unsealed two-block construction including an electronic device unit with four independent channels consisting of electronic and optoelectronic modules and an inertial unit containing four fiber optic gyroscopes.
    Features:
    - precision accuracy;
    - nonsealed double-block construction;
    - MCO or SpaceWire interfaces;
    - no temperature control system.
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    Remark

    Testing phase

    Legal information
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