CT7-8C  
Initial Operational Capability (IOC): 2003
Total Production: ?
Origin: United States of America
Corporations: General Electric
Parent System: T700
Initial Operational Capability (IOC): 1978
Total Production: 20,100
Family Members: CT7, CT7-2, CT7-8, CT7-8E, T700-GE-401, T700-GE-401C, T700-GE-700, T700-GE-701, T700-GE-701C, T700-GE-701D, T700-GE-701E, T700-T6A, T700-T6A1, T700-T6E, T700-T6E1 and T706-GE-700
Reviews
There are no reviews so far

Description: The T700 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.

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.

CT7-8C Applications


Support Aircraft MH-92

CT7-8C Specifications

Power
Max Power at TakeOff: 3,000 shp (2,238 kW)
CEP: Circular Error Probable
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)

CT7-8C News

There is 1 news
on 5 Nov 2015
Thursday, November 5, 2015GE Aviation Delivers 20,000th T700/CT7 Turboshaft Engine

Operators & Related Equipment


OperatorsItems

Grand Total ?1
 
Copyright © 2003-2017 deagel.com website. All rights reserved.
This website has been optimized for HTML 5 and CSS 3.