NIIN Output Data
Definition:
AN ELECTROMECHANICAL AND/OR ELECTRONIC, SELF-CONTAINED, AUTOMATICALLY CONTROLLING DEVICE. IT IS DESIGNED TO BE MOUNTED ON THE BODY OR CONTAINED WITHIN THE GUIDANCE SECTION OF AN AIR LAUNCHED MISSILE. ITS FUNTION IS TO MEASURE LINEAR ACCELERATION, ANGULAR RATE, DELTA-VELOCITY AND DELTA-ALTITUDE. IT CONTAINS SENSORS, ACCELEROMETERS, GYROSCOPES AND THE LIKE. EXCLUDES INERTIAL NAVICATION SYSTEM.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 2922000300 | S5652 | A | 3 | 2 | 5 | ME | ||
| LARC-HY97 | 99999 | A | 6 | 9 | 9 | ZZ |
CAGE Information
| Code | Company |
|---|---|
| 99999 | DEPARTMENT OF DEFENSE AMMUNITION COD |
| S5652 | RAFAEL |
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 |
|---|---|---|
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | PART OF GUIDANCE SECTION; T.O. 21-AG142A-2-1 |
| AGAV | END ITEM IDENTIFICATION | AGM-142A HAVE NAP MISSILE |
| DDAC | DOD AMMUNITION CODE | LARC-HY97 |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | INERTIAL MEASUREMENT UNIT |