| ELECTRICAL POWER SOURCE RELATIONSHIP | OPERATING |
| ENCLOSURE FEATURE | SINGLE ITEM W/CARRYING CASE |
| AC VOLTAGE RATING | 105.0 VOLTS MINIMUM AND 125.0 VOLTS MAXIMUM |
| DEPTH | 25.000 INCHES NOMINAL |
| FREQUENCY RATING | 60.0 HERTZ NOMINAL |
| FUNCTIONAL DESCRIPTION | PERFORMS COMPUTERIZED TEST TO CHECK CRITICAL MISSILE SAFETY AND FLIGHT TERMINATION SYSTEM COMPONENTS PRIOR TO FLIGHT TESTS. PREFORMS POST-BOOST PROPULSION SYSTEM TRANSDUCER TESTS, DESTRUCT SIMULATION RESISTOR FIRING CURRENT TEST AND INTERVAL TIMER AND INERTIA SWITCH TESTS |
| HEIGHT | 10.000 INCHES NOMINAL |
| JOINT ELECTRONICS TYPE DESIGNATION SYSTEM ITEM NAME | TEST SET, MISSILE SYSTEM COMPONENT |
| JOINT ELECTRONICS TYPE DESIGNATION SYSTEM ITEM TYPE NUMBER | AN/GSM-349A |
| MATERIAL AND LOCATION | ALUMINUM HOUSING AND FIBERGLASS CARRYING CASE |
| PHASE | SINGLE |
| REFERENCE DATA AND LITERATURE | JETDAS DD61 USAF-2006-0039-001-001 |
| RELATIONSHIP TO SIMILAR EQUIPMENT | ONE WAY SUBSTITUTEABLE FOR AN/GSM-349 |
| WIDTH | 20.000 INCHES NOMINAL |
| TEST TYPE FOR WHICH DESIGNED | CRITICAL MISSILE SAFETY AND FLIGHT TERMINATION SYSTEM COMPONENTS |