NIIN Output Data
Definition:
A PORTION OF A GUIDED MISSILE SPECIFICALLY DESIGNED FOR SEEKING OUT A TARGET BY DETECTION OF REFLECTED LASER ENERGY. LOCATION OF THE TARGET IS THEN TRANSLATED INTO HOMING COMMAND SIGNALS BY RELATED EQUIPMENT.EXCLUDES SEEKER SECTION, ELECTRO-OPTICAL, GUIDED MISSILE; SEEKER SECTION, INFRARED, GUIDED MISSILE; AND SEEKER SECTION, RADAR, GUIDED MISSILE.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 654054-1 | 82577 | A | 1 | 2 | 1 | ME | ||
| V515-50006-1 | 51215 | A | 3 | 2 | 2 | ME | ||
| AN/DAB-2 | 80058 | M | 5 | 2 | 3 | ME |
CAGE Information
| Code | Company |
|---|---|
| 51215 | BOEING COMPANY THE DBA BOEING DIV DE |
| 82577 | RAYTHEON COMPANY DBA RAYTHEON |
| 80058 | JOINT ELECTRONICS TYPE DESIGNATION S |
Federal Supply Class
Title
GUIDED MISSILE COMPONENTS
Inclusions:
INCLUDES STRUCTURAL COMPONENTS; COMPONENTS AND ACCESSORIES SPECIALLY DESIGNED FOR USE ON OR WITH GUIDED MISSILES, INCLUDING COMPLETE GYRO MECHANISMS, HYDRAULIC PUMPS, AUTOMATIC PILOT MECHANISMS AND SPECIALLY DESIGNED ASSEMBLIES, AND ELECTRONIC GUIDANCE EQUIPMENT INSTALLED IN MISSILES.
Exclusions:
EXCLUDES ELECTRONIC REMOTE GUIDANCE EQUIPMENT USED TO GUIDE MISSILES; SOLID AND LIQUID PROPELLANT UNITS; COMPONENTS OF GYRO MECHANISMS.
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | AGM-65E MISSILE |
| FTLD | FUNCTIONAL DESCRIPTION | SEARCH,DETECT,ACQUIRE,PROCESS AND TRACK LASER ENERGY REFLECTED BY A LASER DESIGNATED TARGET |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | LENGTH 13.00 IN.(PORM 1 INCH) DIAMETER 5.980 IN. MIN,6.020 IN. MAX.; WEIGHT 9 LBS MIN.,11 LBS MAX. |
| TMDN | TYPE/MODEL DESIGNATION | AN/DAB-2 |