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National Stock Number:
2835-01-154-3533
Federal Supply Class:
2835
National Item Identification Number:
011543533
Description:
ENGINE,GAS TURBINE,NONAIRCRAFT
Detail:
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.
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Manufacturer Information:
| 160001-1100 | 55820 | RTX CORPORATION | | 5902924A | 99167 | HAMILTON SUNDSTRAND CORPORATION |
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Techincal Specification:
| FUEL TYPE | JET FUEL | | OVERALL HEIGHT | 16.500 INCHES NOMINAL | | OVERALL LENGTH | 19.500 INCHES NOMINAL | | OVERALL WIDTH | 16.500 INCHES NOMINAL | | MOUNTING TYPE | AIRCRAFT | | POWER OUTPUT FOR WHICH DESIGNED | SHAFT | | 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 |
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