93066: GUIDED MISSILE AND LAUNCHER,SURF.
GUIDED MISSILE AND LAUNCHER,SURF. Key specifications include mounting_style: BRACKET MTD W/THREE MTG HOLES, BOTTOM HOLE THREADED, voltage_in_volts: 12.0, ground_polarity_type: NEGATIVE, shaft_rotation_direction: CLOCKWISE, maximum_output_current_rating_in_amps: 130.0. This part is cataloged in the U.S.
Government catalog under NSN 4920-00-038-1047, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| mounting_style | BRACKET MTD W/THREE MTG HOLES, BOTTOM HOLE THREADED |
| voltage_in_volts | 12.0 |
| ground_polarity_type | NEGATIVE |
| shaft_rotation_direction | CLOCKWISE |
| maximum_output_current_rating_in_amps | 130.0 |
| NSN | 4920-00-038-1047 |
| LENGTH | 16.000 INCHES NOMINAL IN |
| REFERENCE DATA AND LITERATURE | T.O.33D4-6-248-1 |
| HEIGHT | 10.375 INCHES NOMINAL IN |
| SPECIAL FEATURES | 115V AC/60HZ/SINGLE PHASE/22.5V BATTERY/MAX ENERGY MEASUREMENT LEVEL 30.0 JOULES/C/O TESTER,IGNITION EXCITER 1;CABLE ASSY 3 V |
| DEPTH | 11.000 INCHES NOMINAL IN |
| ENCLOSURE FEATURE | MULTIPLE ITEM W/CARRYING CASE |
| END ITEM IDENTIFICATION | J85-5,5A,13 TURBOJET ENGINES A |
| TEST TYPE FOR WHICH DESIGNED | ENGINE IGNITION SYSTEMS |