Mathematical Simulation of Ammonia Electrothermal Fine Adjustment Microthrusters According to Results of Field Tests of Fine Adjustment Thrusters
Annotation
Results of full-scale tests of the ammonia correcting propulsion systems (CPS) as a part of the small spacecraft’s (SSC) are presented, the mathematical simulation of temperature conditions of electrothermal thruster (ETT) of the CPS received on the basis of processing of temperature parameters of natural thrusters with their further forecasting on the maximum period of single inclusion of ETT, a specific impulse of draft of ETT and stocks of characteristic velocity of CPS as a part of SSC is considered.
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