The ASIM experiment on the ISS. Torsten Neubert and the ASIM Team

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Transcription:

The ASIM experiment on the ISS Torsten Neubert and the ASIM Team

Content The Science The ASIM Payload The Science Instruments Status and Consortium 2 DTU Space, Technical University of Denmark

The occurrence of lightning ISS Coverage LIS Data, Hugh Christian 3 DTU Space, Technical University of Denmark

The global transport Ordinary storms: horisontal winds Thunderstorms: vertikal winds Make them electric Transporterer dust and water vapor to high altitude. The higher: longer lifetime larger area affected larger overall effect 4 DTU Space, Technical University of Denmark

But what happens above thunderstorms????? Difficult to measure from ground, balloon and aircraft The mesosphere is also called the ignorosphere Some satellite observations during recent years Tordenstorm over Mali, 5 februar, 2008 set fra ISS 5 DTU Space, Technical University of Denmark

Giants discovered in 2005 Højde (km) 90 80 70 60 50 40 30 20 Patrice Huet Serge Soula, J. Geophysical Research, 2011. 6 DTU Space, Technical University of Denmark

Terrestrial Gamma-ray Flashes TGF - 1994 Fishman et al. Science, 1994 Gjesteland et al., JGR, 2012 7 DTU Space, Technical University of Denmark

ASIM Objectives To study energetic thunderstorm processes X- and Gamma-radiation Lightning from clouds to the ionosphere Cloud and storm development To study Cosmic influences on the atmosphere Lightning initiation stimulated by cosmic radiation Meteor seeding of electric discharges in the mesosphere Energetic particle precipitation from the magnetosphere (aurora) 8 DTU Space, Technical University of Denmark

The ASIM Mission ASIM will be launched by SpaceX Dragon to the International Space Station in 2016 The instruments are mounted outside the ESA Columbus module pointing nadir Observations in bands that are absorbed in the atmosphere Consortium lead is Terma Funding from ESA and national sources ASIM 9 DTU Space, Technical University of Denmark

The Payload MMIA (The Modular Multispectral Imaging Array): three photometers two cameras MXGS (The Modular X- and Gamma-ray Sensor): low-energy detector (LED) high-energy detector (HED) 10 DTU Space, Technical University of Denmark

The MMIA Three photometers: 180-250 nm 337.0 nm/5 nm band 777.4 nm/5 nm band 100 khz sampling Two cameras 337.0 nm/5 nm band 777.4 nm/5 nm band 1 M-pixel 400 m resolution 12 frames/sec event detection software e2v CCD with on-chip amplification MMIA photometer MMIA camera 11 DTU Space, Technical University of Denmark

MMIA in numbers Envelope: Vægt: Power: Data rate: 80.3 x 38.0 x 34.5 cm 17.2 kg 18.7 W + 20 W heaters 17 kbps MMIA on the CEPA 12 DTU Space, Technical University of Denmark

MXGS Exploded View 13 DTU Space, Technical University of Denmark

MXGS Specifications Energy range Energy resolution Quantum efficiency Relative time accuracy Burst rate capability TGF sensitivity (RHESSI mean TGF spectrum) Instrument background Trigger Auroral events peak rate Mounting Fully Coded Field of View Location accuracy (STD error circle) (RHESSI mean TGF spectrum) LED: 15-400 kev HED: 0.2-20 MeV LED: <10% @ 60 kev HED: <15% @ 662 kev LED: >0.94 @ 100keV HED: >0.60 E> 1 MeV < 5 s LED: >350 cts/ms HED: >650 cts/ms LED: S/N > 7 HED: S/N >15 LED: 2.4 cts/ms HED: 2.0 cts/ms Bi-directional link to MMIA 10 6-10 7 cts/s for a few minutes Nadir-pointing LED: 80 O x 80 O HED: N/A Point source: < 0.7 O 3 O diffuse source: <3.0 O 14 DTU Space, Technical University of Denmark

MXGS in numbers Envelope: Vægt: Power: Data rate: 51.8 x 74.6 x 76.8 cm 138.6 kg 107 W 12 kbs MXGS Structural-thermal model at INTA, Madrid 15 DTU Space, Technical University of Denmark

MXGS data modes 16 DTU Space, Technical University of Denmark

MXGS science modes TGF Search Sub-Mode Used in low detector background situations where data relevant to primary science objectives are being collected TGF search algorithms are enabled Monitoring functions of background rates, detector count sampling, accumulation of spectrally-binned data and time-binned data, are enabled. High Background Sub-Mode Entered in high background situations (e.g. SAA passages) TGF search algorithms are disabled and monitoring functions are enabled If the background increases further, the detector enters a grey mode where only a fraction of detector events are recorded, to maintain DPU loading below 75% At very high background levels, data communication to the DPU may be disabled completely. Auroral Capture Sub-Mode Entered in high background situations, outside SAA passages, where data relevant to secondary science objectives are being collected, e.g. Auroral and REP events. Identical to High Background Sub-Mode except that when the detector background rate exceeds a configurable threshold, high time resolution histograms are collected directly from address-mapped registers in the RCUs 17 DTU Space, Technical University of Denmark

ASIM Status Critical design review finished May 2014 PFM Delivery to ESA summer 2015 Launch 12 th May 2016 In orbit for a minimum of 2 years 18 DTU Space, Technical University of Denmark

The ASIM Consortium MMIA Terma MXGS DTU Space DTU Space University of Bergen Space Research Institute, Poland University of Valencia Instrument computers DTU Space Terma Payload computer Carlo Gavvazzi, Italy Facility Science Team Torsten Neubert (DTU Space) Elisabeth Blanc (CEA) Victor Reglero (University of Valencia) Nikolai Østgaard (University of Norway) ASIM International Science Team of 80 groups from 30 countries Including Italy 19 DTU Space, Technical University of Denmark

Optical Observations 20 DTU Space, Technical University of Denmark

The Giant of the Mediterranean --- with a sprite --- Van der Velde et al., 2010 21 DTU Space, Technical University of Denmark

Thank You 22 DTU Space, Technical University of Denmark