Kowasaki TF2: Difference between revisions
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{|{{Infobox Aircraft Begin | |||
|name= TF2 | |||
|image= File:Rd-93.jpg | |||
|caption= | |||
}}{{Infobox Aircraft Engine | |||
|type= [[Turbofan]] | |||
|manufacturer= [[Kowasaki Heavy Industries]] | |||
|national origin= [[Chilokver]] | |||
|first run= | |||
|major applications= [[Nakajima CF-05 Goshawk]] | |||
|produced= | |||
|number built= | |||
|program cost= | |||
|unit cost= | |||
|developed from= | |||
|variants with their own articles= | |||
}} | |||
|} | |||
==Specifications (TF2-20)== | ==Specifications (TF2-20)== | ||
Revision as of 05:07, 5 October 2019
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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: