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Space Power Simulation |
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Typical GEO satellite SAS
27kW maximum power
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Solar Array Simulator
- Master Control Rack with Slave Power Racks
- Can accurately simulate power generated by a solar panel to allow spacecraft testing to be as accurate as possible.
- Can perform both static and dynamic simulations to test spacecraft entering, during, and exiting from an eclipse or simulate a spinning satellite
- Open circuit voltages from 60V Voc to 150V Voc
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Typical scientific satellite SAS 6kW maximum power |
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Next-Generation Power STE/EGSE
This system is sized to accommodate most modern GEO spacecraft.
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Contains Solar Array Simulator, Battery Simulator, Main Bus Power, Secondary Bus Power, Umbilical Power, Launch Support Power, Spacecraft Protection devices, System hardware verification tools, Universal Interface Adapter, and Mains Isolation.
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Operated with single PC running Windows NT or Windows 2000 locally and capable of full remote control via TCP/IP.
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Battery Simulator Systems
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Available in single and dual pack versions
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Sensor simulation available to provide thermistor, strain gauges, heater loads, and cell bypass/short.
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Battery behavior easily modified via spreadsheet download to simulate and battery topology including Nickel Metal Hydride, Lithium Ion, and Nickel Cadmium
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Operated with single PC running Windows NT or Windows 2000 locally and capable of full remote control via TCP/IP.
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Digital Payload Power Rack
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Allows precise power control and monitoring of payload level tests prior to integration with spacecraft.
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Provides multiple DC power sources with data-log monitoring of 40 outputs simultaneously.
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Payload Protection system for over-voltage and over-current.
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Operated with single PC running Windows NT or Windows 2000 locally and capable of full remote control via TCP/IP.
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* System shown is for example only.
All systems and equipment are manufactured in accordance with client specifications.
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