Kuwwat paýlamak we ýylylyk gözegçiligi bölümi
Önümler
Haryt kody |
CG-DJ-PD-100 |
CG-DJ-PD-300 |
Konwertiň ululygy / mm |
94mm × 94mm × 46mm |
150mm × 120mm × 57mm |
Agram |
0,5 kg |
1,3kg |
Kuwwat sarp etmek |
1W |
8.5W (DCDC statiki güýji sarp etmegi goşmak bilen) |
Kuwwat paýlanyşy |
10 kanal 12V / 7 kanal 5.2V |
6 kanal 28V / 8 kanal 12V / 5 kanal 5.2V |
Ateryladyjy zolak bilen dolandyrylýar |
11 kanal, bir kanal üçin iň ýokary 2W |
15 kanal, bir kanal üçin iň ýokary 10W |
Temperatura / Analog giriş maglumatlary ýygnamak |
20 kanal, 12 bitli ýygnamak |
34 kanal, 12 bitli ýygnamak |
Häzir sürmek |
2 kanal |
\ |
Ereýän predohranitel dolandyryş |
2 kanal, häzirki 4 ~ 6A |
2 kanal, häzirki 5 ~ 6A |
Üpjünçilik sikli |
4 aý |
4 aý |
The Power Distribution and Thermal Control Management Unit (PDTCMU) is an advanced system designed to efficiently manage and distribute power while maintaining thermal stability in space-based platforms such as satellites and spacecraft. This unit integrates power distribution, thermal regulation, and system monitoring functions into a single compact module, ensuring the optimal performance of various subsystems onboard. It manages the flow of electrical power from solar panels or batteries to critical satellite components, while also controlling the temperature of sensitive equipment through advanced thermal control systems such as heat pipes, radiators, and thermal insulation. The PDTCMU is equipped with sensors to monitor both power and temperature levels in real-time, enabling dynamic adjustments to maintain the efficiency and reliability of the satellite's systems. It operates under extreme conditions, with robust protection against electrical surges, thermal fluctuations, and radiation, ensuring long-term mission success.
Dolandyryş bölümi. Tehniki aýratynlyklary we bahalary bermegiňizi haýyş edýäris.
Biz bilen habarlaşyň