Spacecraft Electrical Power Systems Test Stand

Project Type: Spacecraft Electrical Power Systems Test Stand

Customer: Lockheed Martin Space

Dynamometer: None

Control System: DynoLAB

Other Equipment: High-voltage Battery/Load Simulators

This system was configured to test spacecraft electrical power and charging systems. By using our high-voltage battery simulator technology, we were able to separately simulate the satellite load power BUS as well as the solar array charging BUS. This system performs 100% quality control testing of the satellite power control modules immediately before integration into the spacecraft.