General
Electric T700/CT7
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| The
Engine |
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Specifications
(CT7-9B) |
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| Introduced
in 1978, the T700 was designed for the U.S. Army's Black Hawk
helicopter with the lessons of Vietnam in mind. The civil CT7
was available in 1984. |
|
 | Turboshaft/Turboprop |
| Compressor: 6-stage |
| Turbine: 2-stage LP/2-stage HP |
| Pressure ratio: 18 |
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| Models |
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Used
by |
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| CT7-9B:
1,750 hp (1305 kW) |
| T700-401: 1,690 hp (1261 kW) |
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| Related
Pages |
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Related
Websites |
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