3. Direct impact with roll. This case is characterized by maximum load on the roll shock absorbers and the largest roll displacement of the spacecraft. At small velocities disengagement is possible if the jet control engines are not used. If the longitudinal shock absorber is not deformed as, for example, in the Soyuz APDA, there remains the equation of rotation of a flywheel on the roll shock absorber The moment of inertia of the flywheel or after conversion The initial angular velocity of deformation of the roll shock absorber is defined by the longitudinal and angular velocities its value may be substantial. Thus for the APDA at and it is equal to . The value of
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