| MRC |
Requirement Statement |
Characteristics |
| ALAS |
INTERNAL CONFIGURATION |
JUNCTION CONTACT |
| CTSG |
MAXIMUM OPERATING TEMP PER MEASUREMENT POINT |
200.0 DEG CELSIUS JUNCTION |
| CTQN |
VOLTAGE RATING IN VOLTS PER CHARACTERISTIC |
120.0 MAXIMUM BREAKDOWN VOLTAGE, COLLECTOR-TO-BASE, EMITTER OPEN AND 120.0 MAXIMUM BREAKDOWN VOLTAGE, COLLECTOR-TO-EMITTER, BASE OPEN AND 4.0 MAXIMUM BREAKDOWN VOLTAGE, EMITTER-TO-BASE, COLLECTOR OPEN |
| ABJT |
TERMINAL LENGTH |
1.500 INCHES MINIMUM |
| CTRD |
POWER RATING PER CHARACTERISTIC |
1.0 WATTS MAXIMUM TOTAL DEVICE DISSIPATION |
| CTRK |
TRANSFER RATIO |
40.0 MINIMUM STATIC FORWARD CURRENT TRANSFER RATIO, COMMON-EMITTER AND 150.0 MAXIMUM STATIC FORWARD CURRENT TRANSFER RATIO, COMMON-EMITTER |
| CTQX |
CURRENT RATING PER CHARACTERISTIC |
1.00 AMPERES MAXIMUM COLLECTOR CURRENT, DC AND 500.00 MILLIAMPERES MAXIMUM BASE CURRENT, DC |
| AGAV |
III END ITEM IDENTIFICATION |
MK 37 GUN FIRE CONTROL SYSTEM; MISSILE, AIR-TO-AIR, SPARROW (AIM-7); MISSILE, AIR-TO-AIR, PHOENIX (AIM-54); SIRIUS CLASS T-AFS 8; HELICOPTER, CARRIER BASED ASW, SH-60F; AIRCRAFT, C-2A (REPROCURED); HELICOPTER, ADVANCE ATTACK, AH-1W; SONAR DOME RUBBER WINDOWS (SDRWS); LANDING CRAFT AIR CUSHION (LCAC); HELICOPTER, MH-53E |
| TTQY |
TERMINAL TYPE AND QUANTITY |
3 UNINSULATED WIRE LEAD |
| ADAV |
OVERALL DIAMETER |
0.370 INCHES MAXIMUM |
| AXGY |
MOUNTING METHOD |
TERMINAL |
| CRTL |
CRITICALITY CODE JUSTIFICATION |
FEAT |
| ALBA |
ELECTRODE INTERNALLY-ELECTRICALLY CONNECTED TO CASE |
COLLECTOR |
| ABHP |
OVERALL LENGTH |
0.260 INCHES MAXIMUM |
| CTMZ |
SEMICONDUCTOR MATERIAL |
SILICON |
| CBBL |
FEATURES PROVIDED |
HERMETICALLY SEALED CASE |
| FEAT |
SPECIAL FEATURES |
WEAPON SYSTEM ESSENTIAL; JUNCTION PATTERN ARRANGEMENT: NPN |
| AYQS |
TERMINAL CIRCLE DIAMETER |
0.200 INCHES NOMINAL |
| ALAZ |
JOINT ELECTRONIC DEVICE ENGINEERING COUNCIL/JEDEC/CASE OUTLINE DESIGNATION |
TO-5 |
| ABBH |
INCLOSURE MATERIAL |
METAL |
