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4130-01-017-0699
Refrigeration Compressor
4130010170699 010170699 9RJ1-0500-TFD-200
A centrifugal, reciprocating, or rotary compressor designed to compress refrigerant gas(es) from an initial intake pressure to a final discharge pressure. It is designed to be driven by an independent power source, such as an electric motor, gasoline or diesel engine, or the like. It does not include the prime mover, condenser(s), external filter-drivers, and the like. It may include various peripheral components such as drive pulley, flexible coupling, and the like. View more Refrigeration Compressor
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Refrigeration Compressor 4130010170699 RQST NE Updated Every Day 4130-01-017-0699 RQST Updated Every
Restrictions 4130-01-017-0699
4130-01-017-0699 is a Refrigeration Compressor that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. The precious metals content of this item is unknown.
End Users 4130-01-017-0699
- NASA (G650)
- Effective Date:
- 1 Apr 1991
Approved Sources 4130-01-017-0699
- Part Number
- Manufacturer
- Status
- 9RJ1-0500-TFD-200
- Manufacturer
- 14569 - Copeland Corp (Obsolete)
- Original Design
- Original Design
Datasheet 4130-01-017-0699
- Characteristic
- Specifications
- Cooling System Design [AAXP]
- Specifications
- Single
- Cylinder Quantity [AAXZ]
- 3
- Stage Quantity [AAYD]
- 1
- Refrigeration Flow Rate In Tons Per Hour [AAYE]
- 7800.0
- Temp Rating Per Function [CSFH]
- 18.3 Deg Celsius Suction
- Special Features [FEAT]
- 440 Vac,3 Phase,60 Hz; 5 Hp Motor
NATO Stock Numbers Related to 4130-01-017-0699
Freight Information 4130-01-017-0699
4130-01-017-0699 has freight characteristics.. 4130-01-017-0699 has a variance between NMFC and UFC when transported by rail and the description should be consulted.