Nanosatellite Platform

Purpose:
<div> </div> <div style="text-align: justify;"> - to control the separation of spacecraft and the offline monitoring of their status in orbit. </div> <div style="text-align: justify;"> - earth remote sensing, detection of earthquake precursors and disaster prevention. </div> <div style="text-align: justify;"> - calibration and adjustment of space monitoring devices, and space debris monitoring. </div> <div> </div> <br>
Year of release: 2020
Guaranteed service life (years): 5
Estimated production / delivery time (months): 18
Flight qualification of the product: No
Brief history of flight qualification:
Production and ground testing of the prototype.
Possibility to adapt the product to customer requirements: Yes


Parameter Value
Working orbits Low, medium and geostationary orbits
Weight of nanosatellite platform 3.5 kg
Weight of payload 1.5 kg
Power supply system capacity (average/peak) (8/20) W
Attiude control Three axial
Attitude control accuracy 10 angular minutes
Power supply voltage 3,2 V (5,0 V)
Overrall dimensions 100 х 100 х 300 mm

Description

Nanosatellite platform.

Remark

Сonfiguration options:

- simple Attitude Control System (ACS) with 3 magnetic torquers (MTs);

- enhanced ACS with 3 MTs, star tracker and

...

Сonfiguration options:

- simple Attitude Control System (ACS) with 3 magnetic torquers (MTs);

- enhanced ACS with 3 MTs, star tracker and 3 reaction wheels;

- maneuvering platform with micro thruster.

Radiation-resistant components.


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