370 likes | 557 Views
Space Environment Measurements by JAXA Satellites and ISS. Takahiro OBARA Space Environment Group Japan Aerospace Exploration Agency (JAXA). 1. 2. Space Environment Effects. CCDs noises. Surface degradation. Solar cell degradation. Electronics degradation. Electrostatic
E N D
Space Environment Measurements by JAXA Satellitesand ISS Takahiro OBARA Space Environment Group Japan Aerospace Exploration Agency (JAXA) 1
Space Environment Effects CCDsnoises Surface degradation Solar cell degradation Electronics degradation Electrostatic Discharge Single Event Phantom commands 3
Space Environment MonitoringSpace Environment Monitoring 5
Radiation Measurements in JAXA MIN MAX MIN MAX MIN MAX MIN QZS1 E T S 6 DRTS ETS-5 M D S 1 ETS-8 E R G Jason-2 Jason-3 ADEOS ADEOS2 ALOS GOSAT ISS/JEM/SEDA-AP Space Environment Monitoring Radiation Belt Model RB Science 7 Warning Information
Radiation Particle Measurement along GTO satellite MDS-1 (2002.2-2003.8) 8
MDS-1 (TSUBASA) Measurement (Obara et al., 2005) 9
MDS-1 (TSUBASA) Measurement (Obara et al., 2005) 10
Seed Electron & plasma wave measurements (Kasahara et al., 2008) 11
MDS-1 MeV electron vs. Akebono VLF MeV electron VLF waves (Obara et al., 2005) 12
2-step acceleration model Intensification of Plasma Waves ② ~keV Hot electrons ① 30~100 keV Seed electrons Wave growth plasma sheet Enhanced convection plasmaspause (Obara et al., 2001) 13
Time evolution of f(K) f3000(K) f0(K) (Omura et al., 2008) 14
New Model Development NASA AE8 MODEL JAXA DYNAMIC MODEL 15
Comparison with Obs. Data MDS-1 Observation JAXA DYNAMIC MODEL 16
Radiation Particle Measurement at GEO satellites DRTS (2002.9- ) ETS-V (1987.8-1997.9 ) 17
Seasonal Variation of MeV Electrons at GEO ETS-8 data (1988-1997) 19
ETS-VMeV electron flux vs. SWsector structure rule SPRING -> Toward AUTUMN -> Away 20
rule SPRING -> Toward AUTUMN -> Away 21
Radiation Particle Measurement at LEO satellites and ISS GOSAT (2009.1- ) ISS/SEDA-AP (2009.7- ) Jason-2(CNES) (2008.6- ) 22
JEM (Japanese Experimental Module) Space Environment Data Acquisition Equipment (SEDA) Exposed Facility Pressurized Module 23
Observation at 400km altitude (Obara et al., 2010) 24
AE8 Model at 400km altitude Significant movement ( or shift ) of intense region 25
Jason-2 1336 km GOSAT 700 km ISS 400 km 26
30keV Electron Data : Jason-2 2010/1/1 - 2010/1/10 2010/4/1 - 2010/4/10 After Large Magnetic Storm on April 5, Large Increase of High Energy Electron Fluxtook place. 28
Injections of 45 keV Electrons were found, which reached down to L=2.3~2.5 (Mlat ~ 50 degree ). This is VERY consistent with Jason-2 data. 29
Simulation / model calculation 30~40 keV Electrons Due to the large convection E fioeld, enegetic electrons approach toward the Earth (Ebihara et al., 2010) 30
Space Environment Measurement at QZSorbit QZS-1 (2010.9- ) QZS-1,2 and 3 31
MAM-S1 POM-S MAM-S2 LPT QZS-1 satellite: TEchnical Data Acquisition Equipments (TEDA) TEDA consist of three parts; (1)Light Particle Telescope:LPT (2)MAgnetoMeter:MAM (3)POtential Monitor:POM With these data, JAXA will identify the cause of the satellite anomaly. 32
0.1MeV 0.8MeV 1 Day QZS-1 Covering Region -QZS-1 Orbit and Electron Flux- over Japan 33
QZS-1 satellite: Altitude: 32000~40000km Projection along the field line Launch; Sept.11, 2010 Line of force Map onto the Earth MAGDAS, SERC, Kyushu Univ. X Earth Radius 34
Data service http://sees.tksc.jaxa.jp 35
electron Space Environment & Effects System (SEES) Real Time Plots WWW Browser System 1. Measurement Data 18 observation data display. Offer to the inside and outside of JAXA 2. Warning mail system Warning notification: X rays, solar proton, and high energy electron 3. Satellite environmental model and analysis tool 90 kinds of space environmental models. Display of satellite environment in 2D and 3D. Observation Data Anik(Canada)E-1、E-2 trouble Useful Tools for Satellite Environment Reseach JAXA SEES URLhttp://sees.tksc.jaxa.jp
END 37