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Temperature-control system simulates space

Tim Dense, Cal-Bay Systems, and Manfred Diehl, Lockheed-Martin Space Systems -- Test & Measurement World, 2/1/2005

 
Fig. 1  A vacuum chamber simulates conditions in space.
Lockheed-Martin Space Systems tests satellite flight hardware in thermal-vacuum chambers. These chambers (Figure 1) simulate the rigors of space using a nitrogen-chilled chamber operating at 1x10–8 Torr vacuum.

The company wanted to replace the unsupported VAX-based hardware that served as the backbone of the system, so its engineers worked with National Instruments to design a dual-chassis PXI-based system (Figure 2) that could control the thermal chambers and perform the necessary tests. Lockheed-Martin then contracted with Cal-Bay Systems, a developer of PC-based measurement and control systems, to make the design a reality.

 
Fig. 2  This thermal system overview depicts power distribution among various component areas.
The final system provided improved test setup, operation, datalogging, and hardware standardization. A residual benefit was that Lockheed's LabView developers leveraged other projects off the new test system to further enhance capabilities.

System description

The Lockheed-Martin thermal-vacuum system consists of a high-vacuum chamber lined with liquid nitrogen cold walls. Radiant solar heat is simulated using 12 resistive heaters operated through a power-distribution system. This power system has a serial interface that controls 12 stepper motor controllers. These motors in turn control a series of autotransformers, which adjust proper power output to the heaters.

Inside the control room, a PXI chassis controller executes the custom Cal-Bay software library application while serving the test data to engineering servers through proprietary datasocket technology. A local SCXI chassis monitors and provides inputs to the control room power distribution control panel by measuring the voltage and current on each heating zone. The chamber pressure reading is also captured by the software for flight hardware safety protection.

System performance

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The new thermal-vacuum system had to be flexible enough to change control-loop feedback channels on the fly and also to change control modes from temperature to power or voltage on the fly. Furthermore, the system had to be robust—automatically switching to backup feedback channels should the primary system malfunction—because the chambers are run 24/7 for extended periods and any breakdown might compromise flight hardware.

To complicate matters, a natural phenomenon called Corona arcing occurs at specific pressures where the dielectric of air ceases to prevent electrical conductivity between heaters and ground. Such a situation can cause electrical arcing capable of destroying flight hardware. By monitoring the system vacuum, the control software must automatically override the power settings to eliminate any harmful electrical potential should vacuum reach the Corona pressure.

 
Fig. 3  A run screen capture displays conditions across several zones.
The new software gives an operator subsecond loop control of any of the 120+ feedback channels including software-configured pseudo channels. A single panel view (Figure 3), gives the operator current operation information and the ability to modify it using the Edit feature. In addition to data-acquisition channels, a pseudo-channel provides control loop feedback with an alarm range that helps engineers ensure that the rate of temperature change for a particular part never exceeds its flight hardware design limitation. The system logs data on thermal conditions by using both sample rates and apertures. Controlling the logging interval plus the dead band range confines dataset size, yet ensures accuracy.

System benefits

By making use of its extensive software libraries, Cal-Bay was able to complete the projected 24 "man months" of work in just four "man months." Also, the system's cost was in line with the industry-standard $100 per channel.

With the new system, Lockheed-Martin has reduced test-commission time, improved operational procedures, and integrated test data into its engineering network. The system provides ultimate operator control with integrated safety features while maintaining subsecond control loops over a widely distributed PXI control system.


Author Information
Tim Dense is project manager and certified LabView developer at Cal-Bay Systems, San Rafael, CA. He holds a chemical engineering degree from U.C. San Diego. tdense@calbay.com.
Manfred Diehl is a test engineer who has worked at Lockheed for the past 24 years. In 2003, he became manager of the space simulation division at Lockheed Missiles & Space in Sunnyvale, CA.

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