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Title | Satellite Power |
Description | We offer standardized batteries and power control units (PCUs) for smallsats. Thanks to our special manufacturing equipment and extensive qualification tests, our products meet the highest |
Keywords | N/A |
WebSite | satellite-power-systems.de |
Host IP | 185.237.65.104 |
Location | - |
Euro€500
Zuletzt aktualisiert: 2022-11-26 16:51:42
satellite-power-systems.de hat Semrush globalen Rang von 0. satellite-power-systems.de hat einen geschätzten Wert von € 500, basierend auf seinen geschätzten Werbeeinnahmen. satellite-power-systems.de empfängt jeden Tag ungefähr 500 einzelne Besucher. Sein Webserver befindet sich in - mit der IP-Adresse 185.237.65.104. Laut SiteAdvisor ist satellite-power-systems.de sicher zu besuchen. |
Kauf-/Verkaufswert | Euro€500 |
Tägliche Werbeeinnahmen | Euro€500 |
Monatlicher Anzeigenumsatz | Euro€500 |
Jährliche Werbeeinnahmen | Euro€500 |
Tägliche eindeutige Besucher | 500 |
Hinweis: Alle Traffic- und Einnahmenwerte sind Schätzungen. |
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satellite-power-systems.de. 7199 IN | A | IP: 185.237.65.104 | |
satellite-power-systems.de. 10800 IN | NS | NS Record: ns01.agenturserver.it. | |
satellite-power-systems.de. 10800 IN | NS | NS Record: ns01.agenturserver.co. | |
satellite-power-systems.de. 10800 IN | NS | NS Record: ns01.agenturserver.de. | |
satellite-power-systems.de. 10800 IN | MX | MX Record: 10 mx2.agenturserver.de. | |
satellite-power-systems.de. 10800 IN | MX | MX Record: 10 mx1.agenturserver.de. | |
satellite-power-systems.de. 10800 IN | MX | MX Record: 20 mx3.agenturserver.de. | |
satellite-power-systems.de. 10800 IN | MX | MX Record: 50 mx4.agenturserver.de. | |
satellite-power-systems.de. 10800 IN | TXT | TXT Record: google-site-verification=chrybul3jMT08QhzQNaGNY56d1R2cNZvTSLICKsau1Y |
Satellite Power Systems by ecarver GmbH Home Products Quality About Us Contact Welcome We offer power subsystems for small satellites. Our focus lies on smallsats in the 20 kg to 100 kg range. Since the power subsystem accomodates many vital spacecraft functions, its design poses a special challenge. This is why we have decided to introduce some standardization for its two main elements, the power control unit (PCU) and the battery . The idea is to improve the reliability of PCUs and batteries and to streamline the manufacturing processes by avoiding their "reeinvention" for every new space mission. We use two different standardization approaches: For the PCU the tailoring for a specific space mission requires much more flexibility, so we work with standard building blocks . For the battery we use what we call a scalable design where the number of cells in series is the only free parameter. Having said all this, we are looking forward to providing you with a tailored power system for |
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