전계방출 전기추진 추력기 연구개발 현황

다국어 초록 (Multilingual Abstract)

As the application of nano-satellites constellation increases worldwide in the wake of New Space era, there is growing demand for the development of thrusters for precise attitude and orbit control of small satellites. Field Emission Electric Propulsion(FEEP) thruster uses a liquid metal as a propellant and accelerates the ionized liquid metal through a strong electric field at the tip of the metal surface. FEEP thruster technology is suitable for nano-satellites which require various missions for attitude and orbit control, because it provides thrust ranging from 1 μN to 1 mN with high specific impulse up to about 10,000 s and can be miniaturized due to its simple structure. In this paper, the basics of FEEP thrusters are introduced, then the current status of research and development of FEEP thrusters are presented.

참고문헌 (Reference)

1 김호락, "전기추력기 연구개발 현황과 동향, Part I: 해외" 한국추진공학회 23 (23): 95-108, 2019

2 문희장, "전기 추진" 한국추진공학회 12 (12): 76-86, 2008

3 Keerl, S, "Two-dimensional plasma plume density characterisation of the IFM Nano Thruster" 2019

4 Tajmar, M., "Threedimensional numerical simulation of fieldemission-electric-propulsion neutralization" 16 (16): 536-544, 2000

5 Tajmar, M, "Three-dimensional numerical simulation of field-emission-electric-propulsion backflow contamination" 38 (38): 69-78, 2001

6 Tajmar, M, "Three-dimensional In-FEEP plasmadiagnostics" 2003

7 Massotti, L, "The ESA Earth Observation Programme activities for the design, development and qualification of the mN-FEEP thruster" 2019

8 Scharlemann, C, "Test results of the qualification tests for the In-FEEP Technology for LISA PF" 2009

9 Tajmar, M, "Survey on FEEP Neutralizer Options" 2002

10 Mueller, J, "Survey of propulsion technologies applicable to cubesats" 2010

11 Scharlemann, C, "Status of the indium FEEP micropropulsion subsystem development for LISA pathfinder" 2007

12 Marcuccio, S, "Slit FEEP thruster performance with ionic liquid propellant" 2013

13 Andersson, B, "SPIS Modeling of FEEP thrusters for LISA Pathfinder" 2007

14 Mühlich, N. S, "Retarding potential analyser development for low density FEEP Thruster beam diagnostics" 2019

15 Polk, J. E, "Recommended practices in thrust measurements" 2013

16 Polk, J. E, "Recommended practice for thrust measurement in electric propulsion testing" 33 (33): 539-555, 2017

17 Scharlemann, C, "Qualification test series of the indium needle FEEP micro-propulsion system for LISA Pathfinder" 69 (69): 822-832, 2011

18 Biagioni, L, "Qualification status of the FEEP-150 electric micropropulsion subsystem" 2005

19 Bock, D, "Plume characterization of NanoFEEP thrusters with a plasma diagnostics facility using carbon-velvet probes" 2017

20 Nicolini, D, "Plume characteristics of the Indium needle emitter (InFEEP) thrusterq" 2001

21 Jelem, D, "Performance mapping and qualification of the IFM Nano thruster EM for in orbit demonstration" 2017

22 Tajmar, M, "Overview of indium LMIS for the NASA-MMS mission and its suitability for an In-FEEP thruster on LISA" 2011

23 Bock, D, "NanoFEEP - Highly Miniaturized FEEP Propulsion System for Attitude and Orbit Control of Cubesats" 2-6, 2016

24 "Morpheus Space"

25 Roussel, J.-F, "Modeling of FEEP plume effects on MICROSCOPE spacecraft" 36 (36): 2378-2386, 2008

26 Tajmar, M, "Miniaturized Indium-FEEP Multiemitter Design and Performance" 2002

27 Mitterauer, J, "Micropropulsion for small spacecraft: a new challenge for field effect electric propulsion and microstructured liquid metal ion sources" 36 (36): 380-386, 2004

28 Ketsdever, A. D, "Micropropulsion for small spacecraft" American Institute of Aeronautics and Astronautics, Inc 2000

29 Marhold, K, "Micronewton thrust balance for indium FEEP thrusters" 2005

30 "M-Space Products"

31 Bharti, M. K, "Literature study of field emission electric propulsion microthruster" 4 (4): 2777-2781, 2017

32 Tajmar, M, "Liquid-metal-ion source development for space propulsion at ARC" 109 (109): 442-446, 2009

33 "Laser Interferometer Space Antenna"

34 Nicolini, D, "LISA Pathfinder field emission thruster system development program" 2007

35 Reissner, A, "Introducing very high Δv Capability to Nanosats and Cubesats" 2015

36 Mitterauer, J, "Indium: An alternative propellant for FEEP-thrusters" 2001

37 Tajmar, M, "Indium field emission electric propulsion microthruster experimental characterization" 20 (20): 211-218, 2004

38 Tajmar, M, "Indium FEEP micropropulsion subsystem for LISA Pathfinder" 2006

39 Tajmar, M, "Indium FEEP Thruster beam diagnostics, analysis and simulation" 2001

40 Marrese-Reading, C, "In-FEEP thruster ion beam neutralization with thermionic and field emission cathodes" 2001

41 Scharlemann, C, "In-FEEP qualification test program for LISA pathfinder" 2008

42 Scharlemann, C, "In-FEEP endurance test for LISA PF" 2009

43 Mühlich, N. S, "IFM Nano Thruster performance studied by experiments and numerical simulations" 54 (54): 095203-, 2020

44 Bock, D, "Highly miniaturized FEEP thrusters for CubeSat applications" 2967498-, 2014

45 Tajmar, M, "High current liquid metal ion source using porous tungsten multiemitters" 111 (111): 1-4, 2010

46 Krejci, D, "Full performance mapping of the IFM Nano Thruster, including direct thrust measurements" 8 : 881-893, 2019

47 Tajmar, M, "Field-Emission-Electric-Propulsion (FEEP)plasma modeling: 3-D full particle simulations" 1999

48 VanderWyst, A. S, "Field Emission Electric Propulsion Thruster Modeling and Simulation" University of Michigan 2006

49 Nicolini, D, "FEEP-5 thrust validation in the 10–100µN range with a simple nulled-pendulum thrust stand: integration procedures" 2001

50 Fernando, W. C. P, "FEEP thruster nano-satellite applications" Cranfield University 2004

51 Rocca, S, "FEEP micro-thrust balance characterization and testing" 17 (17): 711-718, 2006

52 Marcuccio, S, "Experimental performance of field emission microthrusters" 14 (14): 774-781, 1998

53 "Euroconsult’s small-satellite launch forecast"

54 Andrenucci, M, "Endurance Tests of 150 μN FEEP Microthrusters" 2005

55 Massotti, L, "Emerging technologies in the ESA science and earth observation programme" 69-76, 2007

56 "ENPULSION Thruster Comparison Table"

57 Reissner, A, "EFFICIENT DE-ORBITING OF MICRO- AND NANO SATELLITES USING THE IFM NANO THRUSTER" 2017

58 Villemant, M, "Droplets emission from FEEP and colloids thrusters: modelling of droplets dynamics and interaction with spacecraft body" 2019

59 Marhold, K, "Direct thrust measurement of In-FEEP clusters" 2005

60 Nicolini, D, "Direct thrust and thrust noise measurements on the LISA pathfinder field emission thruster" 2009

61 Jelem, D, "Direct thrust and plume divergence measurements of the IFM Nano Thruster" 62 (62): 3398-3404, 2018

62 Schönherr, T, "Development, production, and testing of the IFM nano FEEP thruster" 2019

63 Scharlemann, C, "Development of propulsion means for microsatellites" 2007

64 Vasiljevich, I, "Development of an indium mN-FEEP thruster" 2008

65 Seifert, B, "Development of a low cost PPU for FEEP electric propulsion using cots components" 2016

66 Seifert, B, "Development and verification of a µN thrust balance for high voltage electric propulsion systems" 2013

67 Bock, D, "Development and testing of field emission thrusters at TU dresden" 1-16, 2014

68 Scharlemann, C, "Development and test of an indium FEEP micropropulsion subsystem for LISA pathfinder" 2007

69 Badami, M. A, "Design of a FEEP Thruster for Micro-/Nano-Satellites" Lulea University of Technology 2019

70 Boccaletto, L, "Design and testing of a micro-Newton thrust stand for FEEP" 2000

71 Paolucci, F, "Design and performance study of a micronewton thrust stand for FEEP" 1997

72 Krejci, D, "Demonstration of the ifm nano feep thruster in low earth orbit" 2018

73 Mani, K. V, "Combined chemical-electric propulsion design and hybrid trajectories for stand-alone deep-space CubeSats" 2020

74 Tajmar, M, "Backflow Contamination of Indium Liquid-Metal Ion Emitters (LMIE):Numerical Simulations" 1999

75 Marcuccio, S, "Attitude and orbit control of small satellites and constellations with feep thrusters" 1997

76 Paita, L, "Alta’s FT-150 FEEP microthruster: development and qualification status" 2009

77 Paita, L, "Alta FT-150: the thruster for LISA pathfinder and LISA/NGO missions" 245-249, 2012

78 Tajmar, M, "Advanced 3D Plasma Diagnostic for the Indium FEEP Microthruster" 2003

79 Merkowitz, S. M, "A μNewton thrust-stand for LISA" 19 (19): 1745-1750, 2002

80 Yang, Y.-X, "A torsion balance for impulse and thrust measurements of micro-Newton thrusters" 83 (83): 015105-, 2012

81 Nicolini, D, "3-D plume characterization of a FEEPthruster" 2000

82 Reissner, A, "10 000 h Lifetime Testing of the mN-FEEP Thruster" 2016