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General Electric GE38

Aircraft Engines

The General Electric GE38 is a gas turbine developed by GE Aviation for turboprop and turboshaft applications, and as the T408 it powers the Sikorsky CH-53K King Stallion. It grew out of the GE27, built in the early 1980s under the Army Modern Technology Demonstrator Engines program with a record single-spool pressure ratio of 22 to 1, which lost the V-22 Osprey engine competition. In the late 1980s GE used the GE27 as the basis for turboshaft, turboprop, turbofan and propfan versions under the GE38 name. The T407 military turboprop, made with Lycoming for the Lockheed P-7A, first ran on 26 December 1989 before the P-7 contract was cancelled, and the T408 has a power rating of 7,500 shaft horsepower. The T408 was also flown on a Boeing NCH-47D Chinook testbed.

Facts
Year
1989 1
Displacement or Thrust
T408 power rating of 7,500 shp 1
Classification
Fuel or Cycle
Jet Fuel / Turbine 1
Connections

Of Make

Source General Electric GE38 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source General Electric GE38 (Wikipedia)Lead, maker
Quote, Lead, maker
is a gas turbine developed by GE Aviation for turboprop and turboshaft applications
Sources
1. General Electric GE38 (Wikipedia)
  • Lead, engine kind, cycle
    is a gas turbine developed by GE Aviation for turboprop and turboshaft applications
  • Design and development, T407 first run
    First run on December 26, 1989
  • Design and development, T408 power
    It has a power rating of 7,500 shp
  • Lead, maker
    is a gas turbine developed by GE Aviation for turboprop and turboshaft applications
  • Part Of: Sikorsky CH-53K King Stallion, Lead, application
    It powers the Sikorsky CH-53K King Stallion as the T408
  • Part Of: Boeing CH-47 Chinook, Variants, T408 testbed
    Boeing NCH-47D Chinook (flying testbed)
  • Part Of: Lockheed P-7, Design and development, T407
    for the Lockheed P-7A
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