Svyatobor-1
Cubesat with modified plasma engine «VERА» and thermal imaging camera
The second cubesat of BSTU «VOENMEH» with experimental developments of students
SC name | Horizon |
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NORAD ID | not assigned |
Number in the Register | not assigned |
Call sign | RS59S |
Frequencies | Transmission: 435 MHz, 436 MHz,10 GHz,2.4GHz. Reception: 435 MHz, 436 MHz, 2.4GHz, 863-869 MHz |
Format | 3U |
Weight | 3,2 kg |
Payload | - Electronic Components Research Module; - solar panel deployment system; - orientation system based on flywheel engines; - 3-band transceivers; - camera. |
Mission | Study the effect of radiation on electronic components, tests of an active orientation system based on flywheel engines, photo shooting the Earth's surface, exploring the possibilities of radio lines using linear frequency manipulation and image transmission using fountain codes, studying the degradation of the characteristics of solar panels of various compositions under the influence of space factors |
Platform | Geoscan LLC |
Launch date | is planned for 2024 |
Launch vehicle | |
Status | Waiting for launch |
The «Horizon» smallsat was developed by the team of Baltic State Technical University «Voenmeh» D. F. Ustinov on the basis of the Geoscan 3U satellite platform.
The payload includes:
1) Solar panel module designed to study the degradation of the characteristics of different solar panels under the influence of space factors;
2) Electronic components research module. It includes advanced magnetoresistive random access memory (MRAM) chips, which are tested for stability in conditions of space radiation;
3) The CubeSat mechanical orientation unit, implemented on the basis of electric motors. When controlling the flywheel system, the satellite is oriented along three axes;
4) Payload management system. It consists of transceiver modules operating in the VHF and S bands, and a computing unit with a camera resolution of 3840x2160 pixels.