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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.
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| Powerplant |
| Manufacturer |
GE Aviation
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Powerplant designation
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TG-180
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| Type |
Turbine |
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| Normal Ratings (uninstalled, sea level, static) |
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Max. continuous power
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Intermediate power
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Maximum power
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Take-off power
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| OEI Ratings (uninstalled, sea level, static) |
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OEI Max. continuous power
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OEI Intermediate power
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OEI Contingency power
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OEI 30-second power
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