NSN 1377-00-722-3383 1377M434, 1377-M434, 8597595
Product Details | ROCKET MOTOR
1377-00-722-3383 A nonairbreathing reaction propulsion device that consists essentially of a thrust chamber and exhaust nozzle, and that carries its own solid oxidizer-fuel combination from which hot gases are generated by combustion and expanded through a nozzle. See also ROCKET MOTOR CLUSTER.20413370087Guided Missile and Space Vehicle Explosive Propulsion Units, Solid Fuel; and Components13380083Guided Missile and Space Vehicle Inert Propulsion Units, Solid Fuel; and Components13400048Rockets, Rocket Ammunition and Rocket Components13770056Cartridge and Propellant Actuated Devices and Components
Part Alternates: 1377M434, 1377-M434, 8597595, 1377-00-722-3383, 00-722-3383, 1377007223383, 007223383
Ammunition and Explosives | Cartridge and Propellant Actuated Devices and Components
| Supply Group (FSG) | NSN Assign. | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 13 | 01 JAN 1961 | 00-722-3383 | 21790 ( ROCKET MOTOR ) |
Cross Reference | NSN 1377-00-722-3383
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 8597595 | 19200 | US ARMY ARDEC RDECOM |
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Technical Data | NSN 1377-00-722-3383
| Characteristic | Specifications |
|---|---|
| SIZE DESIGNATION | 33.605 INCH |
| MOTOR PROPELLANT GRAIN QUANTITY | 1 |
| PROPELLANT INHIBITOR | NOT INCLUDED |
| MOTOR PROPELLANT MATERIAL | BALLISTITE |
| PROPELLANT ACCOMMODATION TYPE | DOUBLE BASE-SHEET SOLID |
| MOTOR PROPELLANT GRAIN WEIGHT | 5.8 POUNDS |
| IGNITER | INCLUDED |
| IGNITER INSTALLATION | INSTALLED |
| IGNITER MODEL NUMBER | NOT ASSIGNED |
| CABLE ASSEMBLY CONNECTOR TYPE | INTEGRAL CONTACT |
| CABLE ASSEMBLY MODEL NUMBER | NOT ASSIGNED |
| NOMINAL BURNING TIME IN SECONDS | 0.35 |
| NOMINAL THRUST | 3500.000 POUNDS |
| OVERALL LENGTH | 33.605 INCHES NOMINAL |
| STRAIGHT SECTION OUTSIDE DIAMETER | 2.541 INCHES NOMINAL |
| NOZZLE CANT ANGLE IN DEG | 47.50 |
| WEIGHT | 14.00 POUNDS |
| RESONANCE ROD | NOT INCLUDED |
| DOD AMMUNITION CODE | 1377-M434 |
| SPECIFIC USAGE DESIGN | MODEL M9 AIRCRAFT EJECTION SEAT CATAPULT |
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY MOTOR PROPELLANT GRAIN QUANTITY,MOTOR PROPELLANT GRAIN MODEL NUMBER,PROPELLANT INHIBITOR,MOTOR PROPELLANT MATERIAL,PROPELLANT ACCOMMODATION TYPE MOTOR PROPELLANT GRAIN WEIGHT,OVERALL LENGTH,STRAIGHT SECTION OUTSIDE DIAMETER,NOZZLE CANT ANGLE IN DEG,WEIGHT,UNIT PACKAGE QUANTITY,UNIT PACKAGE TYPE AND PACKAGE MODEL NUMBER |
| III NET EXPLOSIVE WEIGHT | 5.8 TRANSPORTATION POUNDS |
| III HAZARDOUS MATERIAL CLASSIFICATION CODE | 1.3 DEPARTMENT OF DEFENSE HAZARD CLASS DIVISION AND J DEPARTMENT OF TRANSPORTATION CLASS AND C STORAGE COMPATIBILITY GROUP |
| MANUFACTURERS CODE | 19200 |
| DESIGN CONTROL REFERENCE | 8597595 |
Restrictions/Controls & Freight Information | NSN 1377-00-722-3383
| Category | Code | Description |
|---|---|---|
| Hazardous Material Indicator Code | N | There is no data in the HMIS and the NSN is in an FSC not generally suspected of containing hazardous materials |
| Demilitarization Code: | G | Munitions List Item or Commerce Control List Item. Demilitarization required. Ammunition, explosives, and dangerous articles (AEDA). Demilitarization, and if required, declassification and/or removal of sensitive markings or information, will be accomplished. This code will be used for all AEDA items, including those which also require declassification and/or removal of sensitive markings or information. |
| Precious Metals Indicator Code: | U | Precious metal type is unknown |
| Criticality Code: | X | The item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. |
| Automatic Data Processing Equipment: | 0 | Represents items with no ADP components. NOTE: Codes 1 through 6 are only to be used when the item is Automatic Data Processing Equipment (ADPE) in its entirety and is limited to the type meeting only one of the definitions for codes 1 through 6. (See code 9) |
| Category | Code | Description |
|---|---|---|
| No Freight Information | ||