FIELD: devices for test of rocket and small-arms weapons.
SUBSTANCE: the pendulum test stand has a girder with a carriage for attachment of the test object and a carriage displacement detector suspended from its upper bracket through the rotation assemblies. The detector is installed on the upper bracket of the girder and is made in the form of a turn-angle sensor with a pulley on its axle kinematically linked with the pulley fastened on the rotation assembly of the carriage. The diameter of the pulley of the rotation assembly exceeds the diameter of the pulley on the detector axle.
EFFECT: enhanced reliability and reduced error of the impulse of dynamic unbalance at tests of rocket and small-arms weapon.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| RIG FOR DETERMINING THE MOMENTUM AT A SHOT ACTING ON LAUNCHING DEVICE OF SMALL-ARMS OR ROCKET ARMAMENT | 2005 |
|
RU2285220C1 |
| BENCH TO MONITOR PARAMETERS OF AVIATION ROCKET LAUNCH | 2012 |
|
RU2511217C1 |
| BENCH LAUNCHER TO TEST SMALL ARMS OR ROCKETS | 2008 |
|
RU2375662C1 |
| TEST BENCH TO CONTROL AIRCRAFT MISSILE STARTING DEVICE | 2008 |
|
RU2365851C1 |
| TEST BENCH FOR MULTIPLE SIMULATION OF AIR-LAUNCHED MISSILE | 2012 |
|
RU2519596C1 |
| METHOD FOR TEST RIG DEVELOPMENT OF LASER BEAM-CONTROLLED ROCKETS, MICRORANGE AND TEST RIG FOR ITS REALIZATION | 2005 |
|
RU2299475C2 |
| DEVICE FOR DETERMINING PULSE OF ELECTRIC IGNITER POWER | 2014 |
|
RU2568822C1 |
| METHOD AND DEVICE FOR COMPONENT MECHANICAL TESTS | 2010 |
|
RU2442122C1 |
| AUTOMATED PERMANENT FORTIFICATION ROCKET LAUNCHER | 2014 |
|
RU2591561C2 |
| BENCH FOR DYNAMICAL TESTING OF ARTICLES | 2003 |
|
RU2249808C2 |
