METHOD FOR SPACECRAFT MICROACCELERATIONS EVALUATION

摘要

The method is related to the field of space engineering, in particular, to methods for implementation of gravitation-sensitive processes. The objective of the invention is pre-flight evaluation of the design component of microaccelerations. The assessment is performed by means of ground tests of a spacecraft model. The technical result of the invention consists in provision of active monitoring of the microaccelerations level in the zone of process equipment location at an early stage of spacecraft designing. The economical effect of the invention consists in significant reduction of expenses for creation of new space systems possessing unique operational and technical characteristics due to replacement of a part of space flight tests for assessment of microaccelerations level by ground bench tests.