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nce，Atlanta，Georgia，October，2017. [48] GARNER C E，TVERDOKHLEBOV S O，SEMENKIN A V.
[37] BROMAGHIM D R， SALASOVICH R M， LEDUC J R. Evaluation of a 4.5 kW D-100 thruster with anode layer[R].
The electric propulsion space experiment （ESEX）：A demon- AIAA 96-2967，1996.
stration of high power arcjets for orbit transfer applications[J]. [49] MARRESE C M，HAAS J M，DOMONKOS M T，et al. D-
AIP Conference Processing，1988，420：302-307 . 100 performance and plume characteristics on Krypton[C]//
[38] GOELZ T M， AUWETER K M， KURTZ H L. Develop- AIAA Space Program and Technologies Conference，Hunts-
ment and testing of a 100 kW radiation cooled thermal hy- ville，AL，1996.
drogen arcjet thruster[C]//23rd International Electric Propul- [50] JACOBSON D T， JANKOVSKY R. Performance evalua-
sion Conference，Seattle，WA，USA，September，1993. tion of a 50 kW hall thruster[C]//14th Computational Fluid
[39] LITCHFORD R J. High power flex-propellant arcjet perfor- Dynamics Conference，Norfolk，VA，June 28-July 1，1999.
mance[C]//50th Aerospace Science Conference， American [51] CERUTI L，ANTIMIANI A，POLLI A. Power control unit
Institute of Aeronautics and Astronautics， Nashville， Ten- for µN FEEP propulsion subsystem[C]//30th International
nessee，January 9-12，2012. Electric Propulsion Conference，Florence，Italy ，September
[40] HUANG H，PAN W，WU C. Arcjet thruster operated with 17-20，2007.
different propellants[J]. IEEE Transactions on Plasma Sci- [52] PETAGNA C， VALENTIAN D， ROHDEN H V. Field
ence，2011，39（11）：2934−2935. emission electric propulsion （FEEP）：Experimental investi-
[41] KAJI K，SHIBUTANI K，IKEMOTE R，et al. Performance gations on continuous and pulsed modes of operation[C]//
characteristics of direct-current arcjet thrusters use of car- DGLR/AIAA/JSASS 20th International Electric Propulsion
bon dioxide，methane，ammonia，hydrogen，helium，air and Conference，Garmisch-Partenkirchen，W. Germany，October
ice/water etc. in planets and satellites in the solar system to 3-6，1988.
propellants[C]//37th International Electric Propulsion Con- [53] MARCUCCIO S，GENOVESE A，ANDRENUCCIT M. Fie-
ference，Boston，Massachusetts，June，2022. ld emission electric propulsion （FEEP） system study[C]//
[42] BOBER A，MASLENNIKO N. Development and applica- 23rd International Electric Propulsion Conference， Seattle，
tion of electric propulsion thrusters in Russia[C]//23rd Inter- WA，USA，September，1993.
national Electric Propulsion Conference，Seattle，WA，USA， [54] SCHARLEMANN C，GENOVESE A，BULDRINI N，et al.
September，1993. Status of the indium FEEP micropropulsion subsystem de-
[43] ZHURIN V V，KAUFMAN H R，ROBINSON R S. Physics velopment for LISA pathfinder[C]//30th International Elec-
of closed drift thrusters[C]//25th International Electric Pro- tric Propulsion Conference，Florence，Italy September 17-20，
pulsion Conference，Cleveland，Ohio，October，1997. 2007.
[44] KAUFMAN J， HAROLD R. Technology of closed-drift [55] CECCANTI F，PAITA L，CESARI U. 3 200 hours endura-
thrusters[J]. AIAA Journal，1983，23：78-87. nce testing of the Lisa pathfinder FT-150 thruster[C]//31st
[45] LYNN P R，et al. Electric propulsion demonstration mod- International Electric Propulsion Conference， Ann Arbor，
ule （EPDM） flight hall thruster system[C]//25th Interna- MI，USA，September，2009.
tional Electric Propulsion Conference，Cleveland，Ohio，Oc- [56] KREJCI D，REISSNER A. The first 100 FEEP propulsion
tober，1997. systems in space：A statistical view and lessons learnt of 4
[46] SEMENKIN A V， TVERDOKHLEBOV S O， GARKUS- years of ENPULSION[C]//37th International Electric Pro-
HA V I. Operating envelopes of thrusters with anode layer[C]// pulsion Conference，Boston，Massachusetts，June，2022.
27th International Electric Propulsion Conference，Pasadena， [57] GRIMAUD L，SCHONHERR T，VASILJEVICH I. Qualifi-

California，USA，October，2001. cation status update of the MICRO R3 and NANO R3 FEEP
[47] SEMENKI A V， ZAKHARENKOV L E， SOLODUKH- thrusters[C]//37th International Electric Propulsion Confer-
IN A E. Feasibility of high power multi-mode EPS develop- ence，Boston，Massachusetts，June，2022.
ment based on the thruster with anode layer[C]//32nd Inter- [58] GENOVESE A，TAJMAR M，STEIGER W. Indium FEEP
national Electric Propulsion Conference，Kurhaus，Wiesba- endurance test：Preliminary results[C]//27th International El-
den，Germany，September，2011. ectric Propulsion Conference， Pasadena， California， USA，