Kowasaki TF2: Difference between revisions
Jump to navigation
Jump to search
No edit summary |
No edit summary |
||
| Line 19: | Line 19: | ||
|} | |} | ||
The '''Kowasaki TF2''' is a series of afterburning {{wpl|Turbofan|turbofan}} jet engines developed by [[Kowasaki Heavy Industries]]. | |||
==Specifications (TF2-20)== | ==Specifications (TF2-20)== | ||
Revision as of 05:42, 5 October 2019
 | This article is incomplete because it is pending further input from participants, or it is a work-in-progress by one author. Please comment on this article's talk page to share your input, comments and questions. Note: To contribute to this article, you may need to seek help from the author(s) of this page. |
The Kowasaki TF2 is a series of afterburning turbofan jet engines developed by Kowasaki Heavy Industries.
Specifications (TF2-20)
General characteristics
- Type: Afterburning turbofan
- Length: 4.15 m
- Diameter: 1.02 m
- Dry weight: 1135 kg
Components
Performance
- Maximum thrust: 86.37 kN afterburning, 56.75 kN dry
- Bypass ratio: 0.57
- Power-to-weight ratio: