- Design and build an oxygen heat exchanger system to control O2 temps to a small rocket nozzle test article.
- O2 Outlet Temperature Range: 90K to ambient temperature
- O2 Pressure Range: 200 – 2,200 psig
- O2 Flowrate: 0.3 to 30.0 g/s (< 10% that of the PCFS skids at GRC)
- Scope includes 1 week N2 checkout testing/setup at SLI, and 1 week setup/support at Edwards AFB.
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- Heat Exchanger Design
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- Heat Exchanger System Check
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- Heat Exchanger Design
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- Heat Exchanger Control Panel
