Part Details | KEROSENE PROPELLANT
9130-01-644-2509 A propellant consisting of highly refined low aromatic liquid petroleum distillate with a gravity range not exceeding three degrees American Petroleum Institute gravity at 60 degrees fahrenheit (15.56 Celsius). It may contain additives. Excludes KEROSENE; KEROSENE, DEODORIZED; and TURBINE FUEL, AVIATION.
Alternate Parts: M25576RP2 (DRUM), M25576-RP-2 (DRUM), 9130-01-644-2509, 01-644-2509, 9130016442509, 016442509
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 91 | APR 28, 2015 | 01-644-2509 | 22543 ( PROPELLANT, KEROSENE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 9130-01-644-2509
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| M25576-RP-2 (DRUM) | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 9130-01-644-2509
| Characteristic | Specifications |
|---|---|
| MAXIMUM VISCOSITY AT RATED TEMP | 16.5 CENTISTROKES @ -30.00 DEG. F.; |
| MINIMUM FLASH POINT | 140.00 DEG FAHRENHEIT |
| FREEZING POINT MAXIMUM TEMP | -60.00 DEG FAHRENHEIT |
| MILITARY SYMBOL | RP-2 |
| MAXIMUM DISTILLATION END POINT TEMP | 525.00 DEG FAHRENHEIT |
| UNIT PACKAGE QUANTITY | 55.00 |
| UNIT PACKAGE TYPE | B ANY ACCEPTABLE |
| SPECIAL FEATURES | TOTAL SULFUR: 0.1 MG/KG MAX; FREEZING POINT: -60.00 DEG. F.; SPECIFIC GRAVITY: 0.799 TO 0.815; |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | RP-2 ROCKET GRADE KEROSENE PROPELLANT |