2835-12-341-5592

Nonaircraft Gas Turbine Engine Turbine Rotor

2835123415592 123415592 VG95211-ML-123415592 0289 9241

A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the ROTOR, COMPRESSOR, NONAIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, NONAIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, NONAIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, NONAIRCRAFT GAS TURBINE ENGINE. View more Nonaircraft Gas Turbine Engine Turbine Rotor

2835-12-341-5592 ROTOR,TURBINE,NONAIRCRAFT GAS TURBINE ENGINE 2835123415592 123415592

Managed by Germany
NSN Created on 20 Sep 1996
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2835-12-341-5592 ROTOR,TURBINE,NONAIRCRAFT GAS TURBINE ENGINE 2835123415592 123415592 1/1
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2835-12-341-5592 2835123415592 123415592
VG95211-ML-123415592 0289 9241 A single or multistage assembly designed to receive thermal energy from
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2835-12-341-5592 is a Nonaircraft Gas Turbine Engine Turbine Rotor

2835-12-341-5592 End Users End Users 2835-12-341-5592

Germany (ZG)
Italy (ZR)

2835-12-341-5592 Manufacturers Approved Sources 2835-12-341-5592

Part Number
Manufacturer
Status
VG95211-ML-123415592
D3030 - Wehrtechnische Dienststelle Fur (Active)
Definitive Standard
RNCC 2 RNVC 2 DAC 3
0289 9241
D0272 - Rolls-Royce Deutschland Ltd & Co Kg (Active)
Primary Buy
RNCC 3 RNVC 2 DAC 1

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