Chrysler T36D: Difference between revisions
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| name=T36D |
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}}{{Infobox Aircraft Engine |
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|type=Turboprop |
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|manufacturer=Chrysler |
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|national origin=USA |
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|first run= |
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|major applications= |
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|number built=0 |
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==Specifications (variant) == |
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{{jetspecs <!-- If you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] --> <!-- Please include units where appropriate (main comes first, alt in parentheses). If data are missing, leave the parameter blank (do not delete it). For additional lines, end your alt units with )</li> and start a new, fully-formatted line with <li> --> |ref= |type=Turboprop |length= |diameter= |weight= |compressor=Axial |combustion= |turbine= |fueltype= |oilsystem= |power= |thrust=2,500 lb |compression= |bypass= |aircon= |turbinetemp= |fuelcon= |specfuelcon= |power/weight= |thrust/weight= }} |
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==References== |
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Revision as of 06:54, 8 September 2011
| T36D | |
|---|---|
| Typ | Turboprop |
| National origin | USA |
| Manufacturer | Chrysler |
| Number built | 0 |
The Chrysler Chrysler Engineering Corp. T36D Turboprop engine was ordered by the United States Navy in 1948, but was soon deemed unnecessary, and was canceled before any engines were built. It was rated at 2,500 lb thrust.
Specifications (variant)
General characteristics
- Type: Turboprop
- Length:
- Diameter:
- Dry weight:
Components
- Compressor: Axial
Performance
- Maximum thrust: 2,500 lb