270NTA-4-2: SLEEVE,COMPRESSION,TUBE-HOSE FIT.
SLEEVE,COMPRESSION,TUBE-HOSE FIT. Key specifications include material: COPPER ALLOY OVERALL, flow_angle: 90.0 DEGREES, leg_length: 0.520 INCHES NOMINAL SECOND END IN, seat_angle: 20.0 DEGREES FIRST END, thread_class: 2A FIRST END A, connection_type: THREADED INTERNAL PIPE SECOND END. This part is cataloged in the U.S.
Government catalog under NSN 4730-01-113-1791, 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.
| material | COPPER ALLOY OVERALL |
| flow_angle | 90.0 DEGREES |
| leg_length | 0.520 INCHES NOMINAL SECOND END IN |
| seat_angle | 20.0 DEGREES FIRST END |
| thread_class | 2A FIRST END A |
| connection_type | THREADED INTERNAL PIPE SECOND END |
| connection_style | FLARELESS (TUBE) FIRST END |
| operating_pressure | 150.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SINGLE RESPONSE LBS |
| nominal_thread_size | 0.438 INCHES FIRST END IN |
| maximum_operating_temp | 200.0 FAHRENHEIT SINGLE RESPONSE DEGF |
| end_item_identification | HIGH-MOBILITY ARTILLERY ROCKET SYSTEM (HIMARS) |
| media_for_which_designed | AIR SINGLE RESPONSE |
| NSN | 4730-01-113-1791 |
| FLOW ANGLE | 90.0 DEGREES |
| CONNECTION STYLE | FLARELESS (TUBE) FIRST END |
| CONNECTION STYLE | PLAIN (PIPE) SECOND END |
| CONNECTION TYPE | THREADED EXTERNAL TUBE FIRST END |
| CONNECTION TYPE | THREADED INTERNAL PIPE SECOND END |
| NOMINAL OUTSIDE DIAMETER TUBE ACCOMMODATED | 0.250 INCHES FIRST END IN |
| OPERATING PRESSURE | 150.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SINGLE RESPONSE LBS |
| LEG LENGTH | 0.690 INCHES NOMINAL FIRST END IN |
| LEG LENGTH | 0.520 INCHES NOMINAL SECOND END IN |
| NOMINAL THREAD SIZE | 0.125 INCHES SECOND END IN |