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 | ||
|---|---|---|
| Max continuous: | ||
| Take-off / rated: | ||
| Intermediate: | ||
| Maximum: | ||
| OEI Ratings | ||
|---|---|---|
| OEI contingency: | ||
| OEI continuous: | ||
| OEI 30-second: | ||
| OEI intermediate: | ||