NSN 2835-01-561-6850
Part Details | NONAIRCRAFT GAS TURBINE ENGINE
2835-01-561-6850 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: 38083419, 380834-1-9, 2835-01-561-6850, 01-561-6850, 2835015616850, 015616850
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 13, 2008 | 01-561-6850 | 50489 ( ENGINE, GAS TURBINE, NONAIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-01-561-6850
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 380834-1-9 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2835-01-561-6850
| Characteristic | Specifications |
|---|---|
| FUEL TYPE | JET FUEL |
| POWER OUTPUT FOR WHICH DESIGNED | PNEUMATIC |
| REFERENCE DATA AND LITERATURE | 2G-GTCP85-44 |
| SPECIAL FEATURES | TYPE/MODEL DESIGNATION GTCP-180 |
| END ITEM IDENTIFICATION | AM32A-60A |
