Space Platform 50

    • Space Platform 50

    Purpose:
    Design and manufacture of small spacecraft for technological scientific and educational purposes in low circular orbits.
    Year of release: 2012
    Guaranteed service life (years):
    At least 1 year (with bringing SAS up to 5 years).
    Estimated production / delivery time (months): 12
    Flight qualification of the product: Yes
    Brief history of flight qualification:
    The prototype of the platform is part of the ICA "MIR" (launched July 28, 2012).
    Possibility to adapt the product to customer requirements: Yes
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    Parameter Value
    Working orbits Low circular orbit (from 400 to 1500 km) with associated launch
    Platform weight Up to 30 kg
    Payload weight Up to 40 kg
    Payload power supply capacity Average (30 W); peak (90 W) to 10 min.
    Orientation Three-axis, active
    Orientation accuracy, deg ±10
    Nominal voltage, V 27±0,5

    Description

    Platform for small satellites weighing up to 70 kg. the Height of the orbit is 1500 km. Peculiar properties: - untight; - nickel-metal hydride battery (its elements are part of a single onboard control system); - passive thermal control system on heat pipe
    ... Platform for small satellites weighing up to 70 kg. the Height of the orbit is 1500 km.
    Peculiar properties:
    - untight;
    - nickel-metal hydride battery (its elements are part of a single onboard control system);
    - passive thermal control system on heat pipes and heaters;
    - the motion control system of a SPACECRAFT on electromagnetic devices;
    - propulsion system on hydrazine (can also be gas). Installed on demand;
    - a single onboard control system.
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