A continuous combustion type engine. consists primarily of a compressor, aircraft gas turbine engine, chamber, combustion, aircraft gas turbine engine and a turbine assembly, aircraft gas turbine engine. it may have an afterburner, turbine engine and/or 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, pneumatic power or thrust 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.
NSN: 2840-01-326-0215
What are the manufacturers of nsn 2840013260215?
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Does this nsn 2840013260215 have a shelf life? No. This NSN does not have an applicable shelf life. |
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What is the formal definition of nsn 2840013260215 A continuous combustion type engine. consists primarily of a compressor, aircraft gas turbine engine, chamber, combustion, aircraft gas turbine engine and a turbine assembly, aircraft gas turbine engine. it may have an afterburner, turbine engine and/or 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, pneumatic power or thrust 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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Does nsn 2840013260215 contain any precious metals? No precious metal content. |
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Does nsn 2840013260215 contain any hazardous materials? No MSDS. No hazardous material. |
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What is the ESD classification of nsn 2840013260215? No known electrostatic discharge. |
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