Spath Engineering has been involved with two projects testing turbine
engines. Both involved LOX augmentaion of turbine engines with the
purpose of developing an improved platform for flight launched
rockets.
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Images
below show a Jet
Engine research facility built
by Spath Engineering in partnership with MSE Technology Applications of
Butte, Montana and ATK-GASL of Ronkonkoma, New York for the Defense
Advanced Research Projects Agency. Innovative techniques were
applied to a General Electric J85-5 and Pratt and Whitney F100-200 to
extend their Mach number range.
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F100-200
installed in the test position.
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Mass Injection Pre-Compressor Cooling system mounted on the inlet duct
for the F100-200.
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Close-up of the F100-200 mounted on the test stand.
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F100 running augmented (afterburning) at Mojave test site.
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Photos and videos below show
earlier testing with a J-85 turbine engine in New Mexico
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Night
external view of a General Electric J85-5, afterburner operating.
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Video of an internal view of the afterburner in operation taken with
the water-cooled tailpipe camera. The flashing prior to afterburner
lightoff is the igniter plug. The turbine starts to glow as
military power is selected just prior to afterburner lightoff.
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This photo shows the water-cooled tailpipe camera that is able to
internally image the afterburner combustion. The gas in the plume
impinging on the camera probe is around 3,200° F.
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