NSN 2835-01-004-5938
Part Details | NONAIRCRAFT GAS TURBINE ENGINE
2835-01-004-5938 A continuous combustion type engine. Consists primarily of a COMPRESSOR, NONAIRCRAFT GAS TURBINE ENGINE; CHAMBER, COMBUSTION, NONAIRCRAFT GAS TURBINE ENGINE and a TURBINE ASSEMBLY, NONAIRCRAFT GAS TURBINE ENGINE. It may have a fan section. Air is compressed and heated by a combustible fuel and expanded through the turbine. It is designed to furnish a source of rotary shaft and/or pneumatic power. The pneumatic power is obtained by a bleedoff of the engine compressor. For a complete operating power unit, mounted on a base, see POWER UNIT, GAS TURBINE ENGINE.
Alternate Parts: 3811161, 381116-1, 38083411, 380834-1-1, 3808341, 380834-1, GTCP85180, GTCP85-180, 2835-01-004-5938, 01-004-5938, 2835010045938, 010045938
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
28 | JUN 10, 1975 | 01-004-5938 | 50489 ( ENGINE, GAS TURBINE, NONAIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-01-004-5938
Part Number | Cage Code | Manufacturer |
---|---|---|
381116-1 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
380834-1-1 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
380834-1 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
GTCP85-180 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2835-01-004-5938
Characteristic | Specifications |
---|---|
FUEL TYPE | GASOLINE |
OVERALL LENGTH | 36.800 INCHES NOMINAL |
OVERALL HEIGHT | 28.200 INCHES NOMINAL |
OVERALL WIDTH | 26.000 INCHES NOMINAL |
SPECIAL FEATURES | INCLOSURE:INCLUDED; ALTITUDE AT WHICH HORSEPOWER IS RATED:6,098 FT; INLET AIR TEMPERATURE AT WHICH HORSEPOWER IS RATED:130 DEG F; UNPACKAGED UNIT WEIGHT:302 LBS. |
END ITEM IDENTIFICATION | C130 AIRCRAFT, ALLIED SIGNAL INC, MODEL GTCP85-180L |