| MRC |
Requirement Statement |
Characteristics |
| TTQY |
TERMINAL TYPE AND QUANTITY |
3 PIN |
| CSSL |
DESIGN FUNCTION AND QUANTITY |
1 REFERENCE, VOLTAGE, ANALOG |
| CQSZ |
INCLOSURE CONFIGURATION |
CAN |
| FEAT |
SPECIAL FEATURES |
WEAPON SYSTEM ESSENTIAL |
| CZEN |
VOLTAGE RATING AND TYPE PER CHARACTERISTIC |
40.0 VOLTS MAXIMUM POWER SOURCE |
| ADAR |
BODY OUTSIDE DIAMETER |
0.335 INCHES MINIMUM AND 0.370 INCHES MAXIMUM |
| CQSJ |
INCLOSURE MATERIAL |
METAL |
| CWSG |
TERMINAL SURFACE TREATMENT |
SOLDER |
| CRTL |
CRITICALITY CODE JUSTIFICATION |
FEAT |
| CBBL |
FEATURES PROVIDED |
HERMETICALLY SEALED AND HYBRID AND POSITIVE OUTPUTS |
| CQZP |
INPUT CIRCUIT PATTERN |
1 INPUT |
| AFGA |
OPERATING TEMP RANGE |
-55.0 TO 125.0 DEG CELSIUS |
| TEST |
TEST DATA DOCUMENT |
96906-MIL-STD-883 STANDARD (INCLUDES INDUSTRY OR ASSOCIATION STANDARDS, INDIVIDUAL MANUFACTUREER STANDARDS, ETC.). |
| AFJQ |
STORAGE TEMP RANGE |
-65.0 TO 150.0 DEG CELSIUS |
| AGAV |
III END ITEM IDENTIFICATION |
AIRCRAFT, AC-130H, MC-130H, EC-130E, HC-130; AIRCRAFT BOMBER (ATB); HELICOPTER, COBRA/TOW, AH SERIES; SUPPORT EQUIP, C-17A AIRCRAFT; STRATEGIC WEAPON SYSTEMS (POSEIDON AND TRIDENT); AIRCRAFT, PHANTOM F-4; MARINE AIR TRAFFIC CONTROL LANDING SYSTEMS; MISSILE, MINUTEMAN LGM-30; NIMITZ CLASS CVN; HELICOPTER OBSERVATION (AHIP), OH-58D |
| ADAU |
BODY HEIGHT |
0.165 INCHES MINIMUM AND 0.185 INCHES MAXIMUM |
| CTFT |
CASE OUTLINE SOURCE AND DESIGNATOR |
T0-39 JOINT ELECTRON DEVICE ENGINEERING COUNCIL |
| AEHX |
MAXIMUM POWER DISSIPATION RATING |
600.0 MILLIWATTS |
