Saturday, September 06, 2008

T700

IOC: 1978
Total Production: 13,212

T700-GE-700

IOC: 1979
Production: 11,000

Also Known As: CT7

Origin:United States of America

Contractor/s: General Electric

Description: The T700-GE-700 engine was designed for the US Army's UH-60A Black Hawk helicopter as a result of lessons learned in Vietnam. The key requirements of this engine were reliability, operation under adverse environmental conditions and low maintainability.

Specifications
Dimensions: Diameter 400 mm, Length 1,170 mm

Weights: Max Weight 207 kg (456 lb)

Power: Power 1,560 shp

Family Members:
CT7, CT7-8, CT7-8C, CT7-8E, T700-GE-401, T700-GE-401C, T700-GE-701, T700-GE-701C, T700-GE-701D, T700-T6A, T700-T6A1, T700-T6E, T700-T6E1, T706-GE-700 Applications
CT7-8, T700-GE-401, T700-GE-401C, T700-GE-701, T700-GE-701C, T700-GE-701D, T700-T6A, T700-T6A1, T700-T6E, T700-T6E1, UH-60A Blackhawk News
US Army Approves GE for Next Phase Advanced Affordable Turbine Engine Program

Operators

United States of America

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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