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  Electronic / Electrical Test Labs
 

Pratt & Whitney Rocketdyne hosts the world's largest and state-of-the-art Space Power Electronics Laboratory (SPEL), fully equipped EMI/EMC test facility, software test facilities, and environmental test chambers which were specifically designed for testing high voltage space power systems.

   
Test Facilities
 

Space Environmental Test Facility (SETF)

This unique 23,000 sq. ft. test facility supports the power electronics environmental testing of current programs, i.e. ISS, RS-68 and KEW for thermal and vibration testing. Future plans are to support commercial programs, including satellite power and engine controllers.

  • 12 thermal vacuum chambers
  • 5 thermal chambers
  • 2 vibration stations
  • 5000 sq. ft. manufacturing assembly support facility

Space Power Electronics Lab (SPEL)Space Power Electronics Lab (SPEL)

This 10,000 sq. ft. facility with 6,400 sq. ft shield is the most unique power laboratory in the world. It provides a powerful test bed for full performance end-to-end testing. SPEL has been operational since 1989 and is ready and capable of any DC & AC high voltage power electronics testing. The test and measurement capabilities in SPEL includes power output, no-load to full load, efficiency, power quality, power stability, worst case performance, fault tolerance and recovery, voltage and current transfer function, ripple and noise measurement, end-to-end communication and control algorithms, full system integration and evaluation, power system firmware evaluation, step load control and system stability measurement.

SPEL was a major contributor to the International Space Station Power System Integration and Test Program.

  • EMI shielded facility (120db @ 10GHz and 40db @ 10KHz)
  • Dedicated 2,000 KVA power substation with 41,160 to 480 Vac 3 phase power conversion
  • Multi water chiller for equipment
  • Air condition to support 70°F with 300 KVA test bed dissipation
  • Raise floor with under floor cable trays, cold plates to mount system-under-test components
  • Multiple high power 440/280 isolated power feeds
  • ESD qualified
  • Test Environment
    • Air temperature 70 +/- 15 degrees F
    • Cold plate coolant temperature 50 +/- 10 degrees F
    • Support equipment coolant temperature 50 +/- 10 degrees F
    • Battery chamber air temperature 42 +/- 5 degrees F
    • Battery charger cold plate 33 +/- 5 degrees F
    • Pressure ambient air pressure
  • Capable of measurement Total System Performance:
    • AC/DC High Power/High Voltage testing
    • Power output, no-load to full load, mission simulation
    • Power quality, Efficiency, power stability
    • Worst case performance
    • Fault tolerance and recovery
    • End-to-end communication and control algorithms
    • EMI/EMC testing (RE, RS, CE, CS). Fully automated susceptibility testing to 40 GHz and Emissions measurements to 75 GHz. 300 V/m testing to 18 GHz, 20 V/m above 18 GHz
    • Magnetic fielding and arch discharge testing
  • State-of-the-Art Power Test Bed:
    • Test controlled using test scripts or manual methods
    • Computer driven sources, loads, and measurement equipment
    • Computer measurement and presentation tools
 

Electronics Lab

This 1,200 sq. ft. laboratory is an area with unique "World Class" power test ability and is used to develop high voltage power conversion and distribution devices. The area includes:

  • 4 water cooled, cold plate test benches
  • EPO controlled clean isolated power
  • 3-480 volt 200 amp outlets
  • 3-240 volt 50 amp outlets
  • 3-110 volt 50 amp outlets
  • 15-110 volt 20 amp outlets
  • Single point ground grid on wall and floor Halon fire protection
Electronic Development Labs

The Test Equipment Development lab

This 1,800 sq. ft. area is used for final integration and evaluation of Test Support Equipment, breadboard and EM hardware development.

Software Development Lab
  • Test software development platforms
  • PC, Sun, HP & DEC
  • Test software development environments
  • Lab View, Lab Windows, HP Basic, Visual Basic
Test Capabilities
 
  • Power output, no-load to full load mission simulation
  • Efficiency, power quality, power stability
  • Worst case performance
  • Fault tolerance and recovery
  • End-to-end communication and control algorithm
  • Electromagnetic test  ref: EMI site
  • Space power system end to end test
  • Failure detection and analysis
  • Thermal analysis (lasers)
  • Thermal vacuum test
  • Thermal test
  • Vibration test
Personnel and Equipment Safety
 
  • Test teams are CPD, ESD and facility safety certified biannual inspection and re-certification
  • Test abort through "Emergency Power Off" stations
  • Ground fault interrupter for loss of shield ground
  • Water leakage detection circuits in most areas
  • Fire-Halon suppression system with 2 shot capability in shield areas and power sources room