Modified J-35 turbojet. In the XH-17 application the last stages of of the 1-stage compressor were modified by the addition of a plenum duct to direct compressed air to the rotor via a rotating seal.
Normal Ratings | ||
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Max continuous: | ||
Take-off / rated: | ||
Intermediate: | ||
Maximum: |
OEI Ratings | ||
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OEI contingency: | ||
OEI continuous: | ||
OEI 30-second: | ||
OEI intermediate: |