NSN 2835-01-444-3628
Part Details | NONAIRCRAFT GAS TURBINE ENGINE
2835-01-444-3628 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: 380028071, 3800280-7-1, 38002807, 3800280-7, 3800280, DAA3243P003341, DAA3243P003-341, 2835-01-444-3628, 01-444-3628, 2835014443628, 014443628
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 05, 1997 | 01-444-3628 | 50489 ( ENGINE, GAS TURBINE, NONAIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-01-444-3628
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3800280-7-1 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3800280-7 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3800280 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| DAA3243P003-341 | 1W025 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
Technical Data | NSN 2835-01-444-3628
| Characteristic | Specifications |
|---|---|
| FUEL TYPE | JET FUEL |
| POWER OUTPUT FOR WHICH DESIGNED | PNEUMATIC |
| MOUNTING TYPE | AIRCRAFT |
| OVERALL LENGTH | 45.460 INCHES MINIMUM AND 46.460 INCHES MAXIMUM |
| OVERALL HEIGHT | 17.700 INCHES MINIMUM AND 18.700 INCHES MAXIMUM |
| OVERALL WIDTH | 25.500 INCHES MINIMUM AND 26.500 INCHES MAXIMUM |
| REFERENCE DATA AND LITERATURE | AF TO. 1B-2A-4-49 |
| SPECIAL FEATURES | CURRENT TYPE:DC; FURNISHED ITEMS:GEARBOX ASSEMBLY, PERMANENT MAGNETIC GENERATOR, OIL PUMP ASSEMBLY, FUEL CONTROL, PNEUMATIC TURBINE STARTER; INCLOSURE:NOT INCLUDED; AIR FLOW RATE:302.1 LBS PER MINUTE; DISCHARGE PRESSURE RATING:65.77 PSI; VOLTS IN VOLTAGE:22.0 LOWEST 29.0 HIGHEST; NUCLEAR HARDNESS CRITICAL ITEM |
| TEST DATA DOCUMENT | 1W025-D3243P003G SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTING GENERAL TYPE DATA ON CERTAIN ENVIRONMENTAL AND PERFORMANCE REQUIREMENTS AND TEST CONDITIONS THAT ARE SHOWN AS "TYPICAL", "AVERAGE", "NOMINAL", ETC.). |
| SPECIFICATION/STANDARD DATA | 81349-MIL-P-8686 GOVERNMENT SPECIFICATION |
| NONDEFINITIVE SPEC/STD DATA | II TYPE |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | B-2 AIRCRAFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ENGINE ASSEMBLY |
