FIELD: antiaircraft rocket armament. SUBSTANCE: facility to load launcher with rocket in launching tube has fixing pin, rotary lever of pricking mechanism with index pin, socket of electric connector assembly mounted on launching tube and cradles with clamps and locks, plug of electric connector assembly with socket to accommodate fixing pin, mechanism turning lever of launching tube, air-powered motor with extendible rod mounted on frame of launcher. Rod of air-powered motor is hinged to end of crank, the other end of it is put on shaft uniaxially with axle of rotary lever. Moving girder with upper and lower flanges embracing rotary lever and profile protrusion and rest in its upper part is fixed on this shaft. Plug with knife-like shut- off on cheek bordering on moving girder is attached to frame. EFFECT: decreased time for loading of launcher thanks to reduced number of manual operations. 1 cl, 11 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SYSTEM FOR AUTOMATED LAUNCHING OF ROCKETS FROM PORTABLE ANTIAIRCRAFT ROCKET COMPLEX OF "IGLA" TYPE | 2001 |
|
RU2206041C1 |
| ROCKET-TORPEDO LAUNCHER | 1998 |
|
RU2133431C1 |
| TRANSPORT AND LOADING MACHINE | 2000 |
|
RU2194234C2 |
| TRANSPORT-LAUNCHING PACK FOR ROCKETS AND METHOD OF ITS MANUFACTURE | 2000 |
|
RU2166166C1 |
| TWIN LAUNCHER OF ANTI-AIRCRAFT MISSILES OF INDIVIDUAL USE | 1995 |
|
RU2088877C1 |
| PORTABLE ANTITANK ROCKET COMPLEX AND METHOD FOR INSTALLATION OF CONTAINER WITH ROCKET ON LUNCHER | 2003 |
|
RU2243479C2 |
| DEVICE FOR MOVING VERTICALLY TURNABLE SUPPORT BOOM FROM SIDE OF LAUNCH VEHICLE | 2003 |
|
RU2246436C2 |
| AIRCRAFT EJECTION DEVICE | 1999 |
|
RU2145565C1 |
| CARGO DRIVE OF VARYING TRACTIVE FORCE FOR WITHDRAWAL OF SERVICE PLATFORM FROM LAUNCH VEHICLE SIDE | 2000 |
|
RU2182104C2 |
| ROCKET-TORPEDO LAUNCHER | 1999 |
|
RU2148773C1 |
