Spt 70 thruster magnetic
WebSPTs were developed in Russia, and have an extensive flight history, with over 70 thrusters flown since 1971. A joint venture company is qualifying a complete propulsion subsystem … WebInfluence of the magnetic field configuration on the plasma flow in Hall thrusters T Andreussi1,2, V Giannetti1, A Leporini1, M M Saravia1,2 and M Andrenucci1,2 1Space Propulsion Division, SITAEL S.p.A., Pisa, I-56121, Italy 2Department of Civil and Industrial Engineering, University of Pisa, Pisa, I-56122, Italy E-mail: [email protected]
Spt 70 thruster magnetic
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Webthe SPT-140 thruster, three different tests were conducted: an assessment of the performance of the engine at operating points previously tested using two different electrical output filters, an assessment of ... explanation is that the provided magnetic field strength was so far from the optimal value that the axial electron plasma ... Webthe TDU-1 thruster indicated the thruster’s operation became more oscillatory at discharge voltages of ~ 450 V and that the thruster transitioned to a more oscillatory mode at 500 V and 600 V as can be seen in Fig. 2. [13] Detailed plume characterization -1 and TDU-3 thrusters was performed.of the TDU [15,19] Results from the plume
Webwalls, and those with metallic walls (known as a “thruster with anode layer,” or TAL). The type of thruster in this study is the dielectric type. In a Hall thruster, thrust is generated by ionizing and accelerating a propellant, typically a noble gas such as xenon, using perpendicular electric and magnetic fields. As illustrated in Figure 1, a Web30 Sep 2004 · Details. The Russian-designed SPT-100 Hall-effect electrostatic engine of OKB Fakel is the core of the PPS-1350-G supplied by Snecma Moteurs for the SMART-1 …
Webefficiency of 33%–35% [1, 2, 10, 20]. The SPT-70, a flight demonstrated thruster with a maximum operation time of 3100h (∼28kg Xe throughput), produces 40mN of thrust and … WebThe paper presents the research results of the relationship between the magnetic field parameters and geometry characteristics of erosion zones of the discharge chamber insulators of various stationary plasma thrusters (SPT) developed by Experimental Design Bureau “Fakel”, Kaliningrad, Russia.
http://electricrocket.org/IEPC/7059.pdf
WebSPT-70 and SPT-100 were introduced, their thrusts being 40 and 83 mN, respectively. In the post-Soviet Russia high-power (a few kilowatts) SPT-140, SPT-160, SPT-200, T-160 and … the un is another casualty of russia\\u0027s warthe un is ineffectiveWeb27 Apr 2024 · Design of the electric propulsion thruster with power consumption in the range 200 – 300 W. Laboratory testing of designed thruster at two regimes of the discharge power supply operating: а) with discharge voltage … the un is a commiunist orgainsationWebWhen appropriate, boundary conditions were taken from an HPHall model of an SPT-70 Hall thruster. Ion paths within the sheath were also calculated. Results suggest that the radial... the un is a wicked organizationWeb11 May 2024 · The performance of many Hall thrusters has been shown to exhibit sensitivity to background pressure in ground-based test facilities, and this property can have an impact on the prediction of in-space performance. The SPT-140 Hall thruster, similar in design to the SPT-100 thruster, which shows such sensitivity, was subjected to a series of tests to … the un is another casualty of russia\u0027s warWeb13 Mar 2024 · SPT-100 is a Hall-effect ion thruster, part of the SPT-family of thrusters. SPT stands for Stationary Plasma Thruster. It creates a stream of electrically charged xenon ions accelerated by an electric field and confined by a magnetic field. [1] Contents Specifications See also References the un libraryWebA SPT-70 Hall thruster was operated at various conditions and set points to include fine ... that it is strongest in the vicinity of the thruster exit [10]. The magnetic field is chosen to be strong enough to make the electron Larmor radius … the un layers