| 000 | 02161nlm1a2200361 4500 | ||
|---|---|---|---|
| 001 | 644922 | ||
| 005 | 20231030040635.0 | ||
| 035 | _a(RuTPU)RU\TPU\network\10006 | ||
| 035 | _aRU\TPU\network\9720 | ||
| 090 | _a644922 | ||
| 100 | _a20151204a2015 k y0rusy50 ba | ||
| 101 | 0 | _aeng | |
| 135 | _adrcn ---uucaa | ||
| 181 | 0 | _ai | |
| 182 | 0 | _ab | |
| 200 | 1 |
_aDevelopment of a High-Frequency Emissive Probe System for Plasma Potential Measurements in a Hall Thruster _fS. Mazouffre [et al.] |
|
| 203 |
_aText _celectronic |
||
| 300 | _aTitle screen | ||
| 320 | _a[References: p. 34 (26 tit.)] | ||
| 330 | _aA heated emissive probe is a smart diagnostic tool for acquisition of the plasma potential in the discharge and in the plume of a Hall thruster. However, measurements of high-frequency oscillations of the potential require a specific electrical circuit with a low RC time constant. We developed and tested an emissive probe system with a cutoff frequency of 1 MHz. Details about the low-pass filter design as well as first experimental outcomes obtained in the plume of a 200 W permanent magnet Hall thruster are given in this paper. | ||
| 333 | _aРежим доступа: по договору с организацией-держателем ресурса | ||
| 461 |
_tIEEE Transactions on Plasma Science _d1973- |
||
| 463 |
_tVol. 43, iss. 1 _v[P. 29-34] _d2015 |
||
| 610 | 1 | _aэлектронный ресурс | |
| 610 | 1 | _aтруды учёных ТПУ | |
| 701 | 1 |
_aMazouffre _bS. |
|
| 701 | 1 |
_aPetin _bA. |
|
| 701 | 1 |
_aKudrna _bP. |
|
| 701 | 1 |
_aTichy _bM. _cchemist _cProfessor of Tomsk Polytechnic University, Doctor of physical and mathematical sciences _f1947- _gMilan _2stltpush _3(RuTPU)RU\TPU\pers\35771 |
|
| 712 | 0 | 2 |
_aНациональный исследовательский Томский политехнический университет (ТПУ) _bФизико-технический институт (ФТИ) _bКафедра технической физики (№ 23) (ТФ) _h52 _2stltpush _3(RuTPU)RU\TPU\col\18732 |
| 801 | 2 |
_aRU _b63413507 _c20170118 _gRCR |
|
| 856 | 4 | _uhttp://dx.doi.org/10.1109/TPS.2014.2316322 | |
| 942 | _cCF | ||