FIELD: aviation.
SUBSTANCE: in the method of space vehicle (SV) orbital movement correction action during the application of test and corrective actions, the beginning of the engine combustion chamber wall heating steady-state conditions is fixed, the number of the solenoid valves actuations at the inlet to the pressure stabilization unit is recorded, the average rate of the solenoid valves operations and acceleration from the correction engine are determined. Based on the results of working off the correction plans, a set of reliable values of accelerations for further work with the space vehicle is obtained.
EFFECT: providing reliable and operative correction of orbital movement with increasing its accuracy.
1 dwg
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