The Multipurpose Block-Modular Platform

    • The Multipurpose Block-Modular Platform

    Purpose:
    The product: ultra-low-class spacecraft on CubeSat form-factor, as well as nano- and picosatellites is intended for scientific, educational and technological experiments in space. Development of engineering solutions for nanosatellites.
    Year of release: 2015
    Guaranteed service life (years): 5
    Estimated production / delivery time (months): 16
    Flight qualification of the product: No
    Possibility to adapt the product to customer requirements: Yes
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    Parameter Value
    Weight 3U without payload (kg) 2.5
    Dimensions 3U (mm) 100х100х340.5
    Maximum available volume for payload 2.5U
    Power supply voltage and current 6A - 3.3V; 8A - 5V
    Battery capacity (Wh) of power system 140
    Average power for payload (W) 5
    Interfaces for payload UART, SPI, I2C, Ethernet, USB, SpaceWire, CAN, CSI
    Orientation accuracy of magnetic frames / gyrodin (deg.) 10/0.1
    Radio channel speed: basic (kbit/s) and advanced (mbit/s) 0.1-115 and 1.6-100
    Working orbit (km) up to 1500

    Description

    Constructor for assembling nanosatellites from 1U to 12U of the CubeSat form-factor. Dimensions of modules for assembling 100х100х100 mm.
    Features:
    - leaky;
    - a passive thermal control system;
    - on-board subsystems are duplicated and ha
    ... Constructor for assembling nanosatellites from 1U to 12U of the CubeSat form-factor. Dimensions of modules for assembling 100х100х100 mm.
    Features:
    - leaky;
    - a passive thermal control system;
    - on-board subsystems are duplicated and have an independent power supply;
    - optical commutation subsystems;
    - sensors and M-frames as standard;
    - for design of the technological model, equipment in simplified versions is possible.

    The structure of the onboard sub-systems include:
    - on-board control complex "Hydra". Miniature single board computer.

    - on-board radio complex "Polymorph". SDR with two independent transmit/receive channels.

    - system of telemetric control "Inter".
    CCSDS telemetry generation from sensors:
    + temperature sensor;
    + infrared sensor;
    + MEMS three-axis accelerometer-gyroscope-magnetometer;
    + radiation sensor;
    + emission recorder.

    - orientation and stabilization system "Vortex".
    Determination of position in space using the optical sensor, GPS/GNSS. Management of M-frames and gyrodyne.
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    Remark

    The stage of manufacturing prototypes and conducting autonomous tests.

    Legal information
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