&)'( ~10+#"~ * $&) &)% 20153!13 $ 1 Mission &'1D http://tcc.nifty.com/cs/catalog/tcc_schedule/ catalog_080901192852_1.htm 5&'<K. ,FC&';#/E? BM=D6 J &'6 =+* O@I9 ©JAXA ©JAXA < ©JAXA &'A% $)LJ ©JAXA -204 3N"! ©JAXA 2 !:H78(>G ©NASA 2005 • 3 20054 * 20102 20153 x3,x1,x4, !# !# !#x3,x4 10" 700m2 1200m2 1300m2 !#% &1 &1.8 &500 &400 &8,000 /+( 370 '!#3 -2.)$1, 4 '!#2 ! $%'* + &)( • !#" • 5 "#! 10 Hayabusa(2003) Kizuna(2008) Kiku-8 (2006) Midori2(2003) Daichi(2006) Failure investigation Kirari(2005) Himawari-7 (2006) GOSAT(2008) INSAT GCOM(2010) http://www.spacechina.com/ cpyjs_wxyhtq_Details.shtml? recno=48130 ASTRO-G(2012) ©ISRO http://www.ssloral.com/html/satexp/telstar.html India US China 6 10 Multi-Utility Spacecraft Charging Analysis Tool(MUSCAT) • %$$&JAXA • 20073 7 20069'MUSCAT"#! # 10 ISO workshop participants • !"$4=50$$ &0#3 • ISO-11221.*-20118/ • '''',00) +2#;>968: • <?7?(10"$4=50ISO &0% 8 • '' 10 2013 9 10 • – ISO-11221 (2011.7.21) • Space systems -- Space solar panels -- Spacecraft charging induced electrostatic discharge test methods – ISO-11227 (2012.9.11) • Space systems -- Test procedure to evaluate spacecraft material ejecta upon hypervelocity impact – ISO/AWI-19923 • Space environment (natural and artificial) -- Spacecraft potential estimation in worst case environment – ISO/CD-19683 • Space systems -- Design qualification and acceptance tests of small-scale satellite and units seeking low-cost and fast-delivery 10 10& 2010$!#( " 50cmx50cmx50cm50kg%$! '#( 11 10 201023 • • • • • • • • • • • • • 2012 (H2A):HORYU-II (7kg) Launched 2012(H2B to ISS):FIT, Meisei, Wakayama U (all 1.5kg) 2012(PSLV):Proiters (10kg) 2013(Dnepr): WNISAT (10kg) 2014(H2A):Kagoshima U., Kagawa U., Teikyo U., Shinshu U., Tama-art U., Osaka Pref U., Tsukuba U. 2014(H2A) Rising 2 (43kg), UNIFORM-1 (50kg), SOCRATES(50kg), SPROUT (27kg) 2014(Dnepr):Hodoyoshi 3,4 (50kg) 2014(Dnepr):Hodoyoshi-1, QSAT-EOS, TSUBAME, Nagoya-sat (all 50kg) 2014(H2A): Procyon (59kg)Sinen2(15kg)ARTSAT2-DESPATCH(30kg) 2014 ORBIS(50kg) 2014(Cyclone, Brazil):Nano-Jasmine(35kg) Tested at CeNT 2015 CESAT(50kg), HORYU4(10kg), Hodoyoshi 2 (50kg), CHUBUSAT2,3(50kg), UNIFORM2(50kg) 12 2016 ECG, ITF-2, STARS-C, FREEDOM, WASEDA-SAT3, AOBA-VELOXIII 10 • ! HTV ISS Charging sensor Launched on Aug.4, 2013 (2013) (2011-2013) 13 "! 10! • # $%&2012.5.18' 2012.7.11 !"" 14 10 15 (2011) (2013 10=Z-@C DS0<O]R[9 \1U_TBAY b=ZGIVL^ 24W 24> 5;8 9\1U+#+ F<E73 GIM73 .KX, N*Ka*6`*: # (/_ <E<1P? &"AY Q<M +%)')$!<HJ[ 16 %!) • &'$( – %!)* • %!)+ • , • #" 17 <=L9CY&$&"'+BO • <=L9CY-N" # – Q^*CY*.I5cPdU6 • EW_K – HJ<=[g1M;bD RT42 – <=?;5c+a5cEW – ZG#("a!%@V1 eA • <= ,S/_K – `>7ZG\f)+ 68*: ;*FX5<=403 – ]<=S/ 18 *+<'1F0? • $R9;/O • &BAC – J-%G6 !>&BAC/8*+,I • =)K3 – &BAC/8 – *+HN2( • $R "AC – 5E$*+L$ # • 7D/ – )M:QPBL&B@*+.)4D – ()P$R@4D – 5E$7D/ – 19 Laboratory of Spacecraft Environment INteraction Engineering (LaSEINE) 20
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