Monday, September 08, 2008

T700

IOC: 1978
Total Production: 13,212

CT7-8C

IOC: 2003

Origin:United States of America

Contractor/s: General Electric

Description: The CT7-8C is a 3,000-hp class turboshaft engine derived form the proven CT7-8 engine. Its increased power has been achieved through an upgraded high-pressure turbine and a new advanced three-stage low-pressure turbine.

The CT7-8C engine has been selected to power the H-92 Superhawk multi-purpose military helicopter.

Specifications
Power: Power 3,000 shp

Family Members:
CT7, CT7-8, CT7-8E, T700-GE-401, T700-GE-401C, T700-GE-700, T700-GE-701, T700-GE-701C, T700-GE-701D, T700-T6A, T700-T6A1, T700-T6E, T700-T6E1, T706-GE-700 Applications
MH-92

Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
Shaft-Horse-Power (shp)

Last Updated: Sunday, August 24, 2008

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