Part Details | NONAIRCRAFT GAS TURBINE ENGINE
2835-00-004-2653 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: PR0TEUS15M530, 2835-00-004-2653, 00-004-2653, 2835000042653, 000042653
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 07, 1972 | 00-004-2653 | 50489 ( ENGINE, GAS TURBINE, NONAIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-00-004-2653
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| PR0TEUS15M530 | K0378 | ROLLS-ROYCE MILITARY AERO ENGINESLTD |
Technical Data | NSN 2835-00-004-2653
| Characteristic | Specifications |
|---|---|
| FUEL TYPE | F$DCG |
| OVERALL LENGTH | 108.000 INCHES MINIMUM AND 140.000 INCHES MAXIMUM |
| SPECIAL FEATURES | INCLOSURE NOT INCLUDED; POWER OUTPUT FOR WHICH DESIGNED IS A SHAFT; SHAFT HORSEPOWER RATING 3200.0; SHAFT HORSEPOWER RATING SPEED IN RPM 1500.0; ALTITUDE AT WHICH HORSEPOWER IS RATED AT SEA LEVEL 0.0; INLET AIR TEMP AT WHICH POWER IS RATED 80 DEG FAHRENHEIT |