FSC 2845 Rocket Engines and Components
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2845-00-082-9161 2845000829161 | 105604-507 | Adapter, kit, Install | Air Logistics Corporation (01413) | ||
| 2845-00-194-0098 2845001940098 | 8477-470650-11 | Rocket Engine | III End Item Identification: LGM-30 minuteman Criticality Code Justification: AGAV III Part Name Assigned By Controlling Agency: Engine assembly, pitch and yaw | Ampac-ISP Corp. (0BXY0) Lockheed Martin Corporation (80070) | |
| 2845-00-194-0103 2845001940103 | 8477-470670-11 | Rocket Engine | III End Item Identification: LGM-30 minuteman Criticality Code Justification: AGAV III Part Name Assigned By Controlling Agency: Engine assembly, roll | Lockheed Martin Corporation (80070) Ampac-ISP Corp. (0BXY0) | |
| 2845-00-242-9829 2845002429829 | 8477-472009-3 | Retainer, Seal-Tripl | Special Features: Design analysis Criticality Code Justification: FEAT Nuclear Hardness Critical Feature: Hardened | Lockheed Martin Corporation (80070) Textron Systems Corporation (04614) | |
| 2845-00-251-6831 2845002516831 | 10162093 | Release, Propellant Valve, Guided | U S Army Aviation and Missile (18876) | ||
| 2845-00-302-2091 2845003022091 | 8477-470650-15 | Chamber, Thrust, Engine, Pitch and | Special Features: Design analysis III End Item Identification: Engine assembly, pitch and yaw Criticality Code Justification: FEAT | Lockheed Martin Corporation (80070) Textron Systems Corporation (04614) | |
| 2845-00-302-2092 2845003022092 | 8477-47670-15 | Chamber, Thrust | Special Features: Design analysis III End Item Identification: Engine assembly, roll Criticality Code Justification: FEAT | Lockheed Martin Corporation (80070) Textron Systems Corporation (04614) | |
| 2845-00-302-2093 2845003022093 | 8477-471382-1 | Bracket Assembly, Propellant Stor | General Characteristics Item Description: 3.460 in. lg, 4.840 in. W, 0.665 in. thk | Textron Systems Corporation (04614) Lockheed Martin Corporation (80070) | |
| 2845-00-302-2094 2845003022094 | 8477-473104-1 | Fitting, Tube, Dummy Transducer | Special Features: Design analysis Criticality Code Justification: FEAT General Characteristics Item Description: 0.980 in. W, 0.980 in. lg, 1.436 in. H | Lockheed Martin Corporation (80070) Textron Systems Corporation (04614) | |
| 2845-00-313-4874 2845003134874 | RS000155-001-00 | Ring, Split, Axial Engine | III End Item Identification: Engine, axial | Pratt & Whitney Rocketdyne Inc. (02602) | |
| 2845-00-313-4875 2845003134875 | RS000186-001-00 | Ring, Gimbal, Axial Engine | Special Features: Design analysis III End Item Identification: Axial engine Criticality Code Justification: FEAT | Pratt & Whitney Rocketdyne Inc. (02602) | |
| 2845-00-402-0754 2845004020754 | PA850-150-17575 8477-472065-7 | Transducer, Pressure | Lockheed Martin Corporation (80070) Gulton-Statham Transducers Inc. (57187) | ||
| 2845-00-402-0763 2845004020763 | 8477-472009-1 | Retainer, Seal-Triple, low Thrust | III End Item Identification: Minute man, LGM-30 General Characteristics Item Description: Corrosion resistant steel, MIL-S4043 | Lockheed Martin Corporation (80070) Textron Systems Corporation (04614) | |
| 2845-00-406-5844 2845004065844 | 8477-471400-11 8477-471400-13 | Propellant Storage | Special Features: Dot reg no. EX-8808520 III End Item Identification: Minute man, LGM-30 III Dot Identification Number: UN1244 | Lockheed Martin Corporation (80070) Ampac-ISP Corp. (0BXY0) | |
| 2845-00-406-5845 2845004065845 | 8477-471401-13 8477-471401-35 8477-471401-37 8477-471401-11 | Propellant Storage | Special Features: Dot reg no. EX-8808521 III End Item Identification: Minute man, LGM-30 III Dot Identification Number: UN1067 | Lockheed Martin Corporation (80070) Ampac-ISP Corp. (0BXY0) | |
| 2845-00-450-4763 2845004504763 | RS000200-001-06 | Rocket Engine | Fuel/Oxidizer Feed System Type: Pressure Fuel/Oxidizer Tank: Not included Cooling System Type: Transpiration | Pratt & Whitney Rocketdyne Inc. (02602) | |
| 2845-00-458-8802 2845004588802 | RS000192-005-00 | Mount, Thrust Axial | Special Features: Design analysis Criticality Code Justification: FEAT Nuclear Hardness Critical Feature: Hardened | Pratt & Whitney Rocketdyne Inc. (02602) | |
| 2845-00-458-8804 2845004588804 | RS000202-003-00 | Insulator, Valve-Axial Engine | III End Item Identification: LGM-30 minute man General Characteristics Item Description: Titanium sheet, AMS4911 | Pratt & Whitney Rocketdyne Inc. (02602) | |
| 2845-00-458-8813 2845004588813 | 5473-1 ST1520001RES001 | Pad, Met-l-Flex | National Pipe Co. (88797) Pratt & Whitney Rocketdyne Inc. (02602) Barry Wright Corporation (81860) | ||
| 2845-00-458-8814 2845004588814 | 010-50250-2 ST2840004RE0002 | Valve Assembly, Bipropellant | Special Features: Design analysis III End Item Identification: Aerojet engine, LR-87, LR-91 Criticality Code Justification: FEAT | Pratt & Whitney Rocketdyne Inc. (02602) Moog Inc. (94697) |