The analysis of influence of elastic deformations of the space vehicle on distortion of the form of reflecting surfaces of large-sized elements of the design

The opportunity of use of the traditional equations of elastic space vehicle movement for calculations of root-mean-square deviations ofreflecting surfaces is analyzed and the method of calculations of change of geometrical characteristics of reflectors (linear and angular displacements of top and changes of a focal length), caused by elastic deformations of their designs is submitted.