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
Displacement or ThrustT408 power rating of 7,500 shp 1 Classification
Fuel or Cycle 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, makerQuote, 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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