RIG FOR CONTROL OF SEPARATION OF ZERO AND SUSTAINER STAGES OF GUIDED MISSILES Russian patent published in 2005 - IPC

Abstract RU 2253097 C1

FIELD: test equipment, mainly applicable for rig control of guided missiles with parts separated in flight.

SUBSTANCE: the control rig has a foundation, flexible couplings for suspension of the stages of the missile under test, longitudinal couplings for connection of the missile stages to the foundation and a longitudinal loading mechanism, it is provided with two pairs of diametrically opposite oriented transverse flexible couplings located in the plane of suspension for connection of the sustainer and zero stages to the foundation and an additional transverse flexible coupling for connection by means of a tensioning mechanism of the sustainer stage in the area of its control to the foundation, one of the suspensions is connected in the plane of the missile center of mass, the second - in the center of mass of the sustainer stage, and the longitudinal loading mechanism is made in the form of a drum fastened on whose surface is one of the flexible longitudinal couplings, installed in the axis of rotation and provided with a double-arm lever, installed on whose opposite arms are a load and a balance weight that is provided with a retainer of forced release; the rigidity of the diametrically opposite oriented flexible couplings and the points of their application are selected from the respective condition.

EFFECT: provided research of the process of separation of the object of tests in the maximum flight simultaneous conditions.

6 cl, 2 dwg

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RU 2 253 097 C1

Authors

Visjashchev A.V.

Zaval'Njuk A.G.

Kolotilin V.I.

Osin A.I.

Dates

2005-05-27—Published

2004-05-05—Filed