Rocket Engines and Components: 8477-471401-13, RS000200-001-06, ST1520001RES001
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 8477-471401-13 847747140113 | 2845-00-406-5845 | Propellant Storage | Special Features: Dot reg no. EX-8808521 III End Item Identification: Minute man, LGM-30 III Dot Identification Number: UN1067 | Ampac-ISP Corp. (0BXY0) Lockheed Martin Corporation (80070) | |
| 8477-471401-35 847747140135 | 2845-00-406-5845 | Propellant Storage | Special Features: Dot reg no. EX-8808521 III End Item Identification: Minute man, LGM-30 III Dot Identification Number: UN1067 | Ampac-ISP Corp. (0BXY0) Lockheed Martin Corporation (80070) | |
| 8477-471401-37 847747140137 | 2845-00-406-5845 | Propellant Storage | Special Features: Dot reg no. EX-8808521 III End Item Identification: Minute man, LGM-30 III Dot Identification Number: UN1067 | Ampac-ISP Corp. (0BXY0) Lockheed Martin Corporation (80070) | |
| 8477-472009-1 84774720091 | 2845-00-402-0763 | 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) | |
| 8477-472009-3 84774720093 | 2845-00-242-9829 | Retainer, Seal-Tripl | Special Features: Design analysis Criticality Code Justification: FEAT Nuclear Hardness Critical Feature: Hardened | Lockheed Martin Corporation (80070) Textron Systems Corporation (04614) | |
| 8477-472065-7 84774720657 | 2845-00-402-0754 | Transducer, Pressure | Lockheed Martin Corporation (80070) | ||
| 8477-473104-1 84774731041 | 2845-00-302-2094 | 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) | |
| 8477-47670-15 84774767015 | 2845-00-302-2092 | 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) | |
| A0413006 | 2845-01-524-2411 | Assembly, Dc Motor | End Item Identification: Minuteman III missle Part Name Assigned BY Controlling Agency: Motor assy Special Features: Psre rocket propulsion system | Aerojet-General Corporation (3BXS5) | |
| LR58RM4 | 2845-00-801-7532 | Rocket Engine | ATK Tactical Systems Company LLC (07299) | ||
| PA850-150-17575 PA85015017575 | 2845-00-402-0754 | Transducer, Pressure | Gulton-Statham Transducers Inc. (57187) | ||
| R023068-521 R023068521 | 2845-01-239-5282 | Axial Engine Assembly | III End Item Identification: Peacekeeper stage iv | Pratt & Whitney Rocketdyne Inc. (02602) | |
| R023080-121 R023080121 | 2845-01-194-4497 | Rocket Engine | Special Features: Hardness critical item Criticality Code Justification: FEAT Fuel/Oxidizer Feed System Type: Pressure | Pratt & Whitney Rocketdyne Inc. (02602) | |
| RS000155-001-00 RS00015500100 | 2845-00-313-4874 | Ring, Split, Axial Engine | III End Item Identification: Engine, axial | Pratt & Whitney Rocketdyne Inc. (02602) | |
| RS000186-001-00 RS00018600100 | 2845-00-313-4875 | Ring, Gimbal, Axial Engine | Special Features: Design analysis III End Item Identification: Axial engine Criticality Code Justification: FEAT | Pratt & Whitney Rocketdyne Inc. (02602) | |
| RS000192-005-00 RS00019200500 | 2845-00-458-8802 | Mount, Thrust Axial | Special Features: Design analysis Criticality Code Justification: FEAT Nuclear Hardness Critical Feature: Hardened | Pratt & Whitney Rocketdyne Inc. (02602) | |
| RS000200-001-06 RS00020000106 | 2845-00-450-4763 | Rocket Engine | Fuel/Oxidizer Feed System Type: Pressure Fuel/Oxidizer Tank: Not included Cooling System Type: Transpiration | Pratt & Whitney Rocketdyne Inc. (02602) | |
| RS000202-003-00 RS00020200300 | 2845-00-458-8804 | Insulator, Valve-Axial Engine | III End Item Identification: LGM-30 minute man General Characteristics Item Description: Titanium sheet, AMS4911 | Pratt & Whitney Rocketdyne Inc. (02602) | |
| SM-C-969482 SMC969482 | 2845-01-287-8926 | Counterweight | General Characteristics Item Description: Tungsten, MIL-T-21014 ty 2 cl 2; 1.120 in. od; 0.2755 in. min 0.2757 in. max dia center hole; 0.188 in. min 0.192 in. max thk | US Army Communications (80063) | |
| ST1520001RES001 | 2845-00-458-8813 | Pad, Met-l-Flex | Pratt & Whitney Rocketdyne Inc. (02602) |