Further Development of the JT15D Turbofan
730919
02/01/1973
- Event
- Content
- When United Aircraft Corp.'s JT15D engine was first considered for potential high-altitude, low flight speed, long-endurance RPV applications by the U.S. Air Force, the questions were:
- 1.Will the engine run at these altitudes?
- 2.Can it deliver the required thrust?
- 3.Can it deliver the required power extraction?
- 4.What is the specific fuel consumption?
- 5.What oil system modifications are needed?
- 6.What is the optimum control system?
- 7.Are there other unknowns?
A JT15D-4 turbofan engine, with only minor modifications which were easily incorporated into engines coming off the production line, proved more than adequate to achieve predicted endurance goals and measured performance. - 1.
- Pages
- 14
- Citation
- Anschutz, R., and Cook, D., "Further Development of the JT15D Turbofan," SAE Technical Paper 730919, 1973, https://doi.org/10.4271/730919.