Further Development of the JT15D Turbofan

730919

02/01/1973

Event
National Aerospace Engineering and Manufacturing Meeting
Authors Abstract
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. 1.
    Will the engine run at these altitudes?
  2. 2.
    Can it deliver the required thrust?
  3. 3.
    Can it deliver the required power extraction?
  4. 4.
    What is the specific fuel consumption?
  5. 5.
    What oil system modifications are needed?
  6. 6.
    What is the optimum control system?
  7. 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.
Meta TagsDetails
DOI
https://doi.org/10.4271/730919
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.
Additional Details
Publisher
Published
Feb 1, 1973
Product Code
730919
Content Type
Technical Paper
Language
English