National Stock Number (NSN) Output Data
Definition:
AN INERT ITEM CORRESPONDING IN FORM AND SIZE TO A PROPULSION SECTION, GUIDED MISSILE. IT DOES NOT CONTAIN INTERNAL FUNCTIONAL PARTS AND IS DESIGNED TO DEVELOP SKILL IN THE TECHNIQUES REQUIRED FOR THE ASSEMBLY OF THE PROPULSION SECTION WITH OTHER SECTIONS OF A DUMMY GUIDED MISSILE; DUMMY GUIDED MISSILE (AS MODIFIED); OR DUMMY GUIDED BOMB. IT MAY ALSO BE USED AS A DUMMY ON OTHER GUIDED MISSILES OR GUIDED BOMBS.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| VM020002-101 | 51215 | A | 3 | 2 | 2 | ME | ||
| WPU-9(D-2)/B | 07878 | M | 5 | 2 | 2 | ZZ | ||
| 1338-AY68 | 99999 | A | 6 | 9 | 9 | ZZ |
CAGE Information
| Code | Company |
|---|---|
| 07878 | AERONAUTICAL AND SUPPORT EQUIPMENT T |
| 51215 | BOEING COMPANY THE DBA BOEING DIV DE |
| 99999 | DEPARTMENT OF DEFENSE AMMUNITION COD |
Federal Supply Class
Title
GUIDED MISSILE AND SPACE VEHICLE
Inclusions:
INCLUDES ROCKET MOTORS (SOLID PROPELLANT UNITS) FOR GUIDED MISSILES, INERT-LOADED OR EMPTY; ALL INERT (NONEXPLOSIVE) COMPONENTS FOR GUIDED MISSILE AND SPACE VEHICLE SOLID FUEL PROPULSION UNITS.
Exclusions:
EXCLUDES ROCKET MOTORS (SOLID PROPELLANT UNITS) FOR GUIDED MISSILES, EXPLOSIVE-LOADED; GUIDED MISSILE WARHEADS AND COMPONENTS; ROCKET PROPULSION UNITS; ROCKET MOTORS (SOLID PROPELLANT UNITS) FOR ROCKETS.
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| ADAV | OVERALL DIAMETER | 9.000 INCHES NOMINAL |
| DDAC | DOD AMMUNITION CODE | 1338-AY68 |
| ABHP | OVERALL LENGTH | 127.500 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | USED ON DUMMY GUIDED MISSILE DATM-130A LOAD CREW TRAINER;WITH F-4E AND F-111F ACFT |
| AKYD | ACCESSORY COMPONENTS AND QUANTITY | ROCKET MOTOR INERT 1EA;NOSE FAIRING 1EA;MOTOR ATTACH FITTING 1EA;SEPERATION SYSTEM-THRUSTER 1EA;POWER CARTRIDGE INERT 1EA |
| TMDN | TYPE/MODEL DESIGNATION | WPU-9(D-2)/B |
| FEAT | SPECIAL FEATURES | BODY DIA 9.0 IN EXCLUD ATTACH POINTS AND VENTRAL FIN;LENGTH 127.5 IN;WEIGHT 490 LBS;MATL: MOLDED FIBERGLASS,ALUMINUM,STEEL,COPPER;CONTAINS 1 ROCKET MOTOR,INERT HT006569;1 NOSE FAIRING VM022081-001;1 MOTOR ATTACH FITTING AFT VM022006-003;1 SEPARATION SYSTEM-THRUSTER VE325-5002-001, POWER CARTRIDGE,INERT VE325-5003-002 |