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Journal Science Intensive Technologies №8 for 2016 г.
Article in number:
Firing tests bench for plasma thrusters in JSC «ISS»
Keywords: propulsion subsystem stationary plasma thruster firing test vacuum chamber flowmeter control system test and control equipment
Authors:
A.V. Nikipelov - Head of Group, JSC Academician M.F. Reshetnev «ISS» (Zheleznogorsk). E-mail: niki@iss-reshetnev.ru R.S. Simanov - Leading Engineer, JSC Academician M.F. Reshetnev «ISS» (Zheleznogorsk). E-mail: simru@iss-reshetnev.ru Yu.M. Ermoshkin - Head of Laboratory, JSC Academician M.F. Reshetnev «ISS» (Zheleznogorsk). E-mail: erm@iss-reshetnev.ru E.N. Yakimov - Main Designer, JSC Academician M.F. Reshetnev «ISS» (Zheleznogorsk). E-mail: yen@iss-reshetnev.ru V.V. Maksimov - Head of Sector, JSC Academician M.F. Reshetnev «ISS» (Zheleznogorsk). E-mail: maksimov@iss-reshetnev.ru A.K. Sharov - Head of Department, JSC Academician M.F. Reshetnev «ISS» (Zheleznogorsk). E-mail: sharov@iss-reshetnev.ru
Abstract:
While integrating the propulsion subsystem equipment into spacecraft the most objective prover of the system availability is conducting of firing tests of plasma thrusters together with the conversion and control system and equipment for working body feed. To perform such kind of tests the adequate experimental facility is required. Firing tests bench has been produced in JSC «ISS». The given article is dedicated to the description of characteristics concerning the firing test bench and corresponding equipment.
Pages: 61-66
References

 

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