NSN 2835-01-154-3533
Part Details | NONAIRCRAFT GAS TURBINE ENGINE
2835-01-154-3533 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: 5902924A, 1600011100, 160001-1100, 2835-01-154-3533, 01-154-3533, 2835011543533, 011543533
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 24, 1983 | 01-154-3533 | 50489 ( ENGINE, GAS TURBINE, NONAIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-01-154-3533
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5902924A | 99167 | HAMILTON SUNDSTRAND CORPORATION |
| 160001-1100 | 55820 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
Technical Data | NSN 2835-01-154-3533
| Characteristic | Specifications |
|---|---|
| FUEL TYPE | JET FUEL |
| POWER OUTPUT FOR WHICH DESIGNED | SHAFT |
| MOUNTING TYPE | AIRCRAFT |
| OVERALL LENGTH | 19.500 INCHES NOMINAL |
| OVERALL HEIGHT | 16.500 INCHES NOMINAL |
| OVERALL WIDTH | 16.500 INCHES NOMINAL |
| REFERENCE DATA AND LITERATURE | AF TO. 2JA3-57-3 |
| SPECIAL FEATURES | MAX ALLOWABLE ENG SPEED 67722.0 RPM; CCW ROTATION; MAX RATED EXHAUST GAS TEMP 1200 DEG F; MAX EXHAUST GAS TEMP DURING START 1385 DEG F; FUEL STD MIL-T-5624, TY JP4/5; SINGLE-STAGE CENTRIFUGAL-FLOW COMPRESSOR; SINGLE-STAGE RADIAL-INFLOW TURBINE; ANNULAR COMBUSTOR; CAPACITOR-DISCHARGE TY INGITION EXCITER; SURFACE-DISCHARGE TY SPARK PLUG |
| END ITEM IDENTIFICATION | F-16 ACFT |