CONCORDIASI - umr-cnrm.fr8 SPB Technical Challenges Balloon design and operations Envelope Strength...
Transcript of CONCORDIASI - umr-cnrm.fr8 SPB Technical Challenges Balloon design and operations Envelope Strength...
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AtmosphericAtmospheric ScienceLong duration stratospheric balloon experiment
Sept 2010 – January 2011
CONCORDIASIAntarctica
Overview of the measurement campaign
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CONCORDIASIPresentation outline
Super Pressure Balloon
Concept
Mission
Technical challenges Balloon Infrastructure and launch
process On board systems Flight monitoring and control Rapid distribution of scientific
data
CONCORDIASIScientific investigatorsMeasurement planLaunch campaignFlight overviewDriftsondesIn situ measurement
1 – Ozone destruction2 – Ozone
depletion/replenishment 3 – Stratospheric Dynamics -
waves
Experiment• Atmospheric sounding
through GPS occultation
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CONCORDIASIPresentation outline
Super Pressure Balloon
Concept
Mission
Technical challenges Balloon Infrastructure and launch
process On board systems Flight monitoring and control Rapid distribution of scientific
data
CONCORDIASIScientific investigatorsMeasurement planLaunch campaignFlight overviewDriftsondesIn situ measurement
1 – Ozone destruction2 – Ozone
depletion/replenishment 3 – Stratospheric Dynamics -
waves
Experiment• Atmospheric sounding
through GPS occultation
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Super-Pressure Balloonsconcept
Zero Pressure Balloon Open balloon (venting ducts)Can fly high with heavy loadsShort duration (except special conditions…)
Super-Pressure balloon Sealed balloonLowermost stratosphere, light loadsLong duration flights
Photo courtesy Jack Fox
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CONCORDIASIPresentation outline
Super Pressure Balloon
Concept
Mission
Technical challenges Balloon Infrastructure and launch
process On board systems Flight monitoring and control Rapid distribution of scientific
data
CONCORDIASIScientific investigatorsMeasurement planLaunch campaignFlight overviewDriftsondesIn situ measurement
1 – Ozone destruction2 – Ozone
depletion/replenishment 3 – Stratospheric Dynamics -
waves
Experiment• Atmospheric sounding
through GPS occultation
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Super-Pressure Balloons Mission
Flights of several months in the lowermost stratosphere, quasi-lagrangian observations of the local air parcel
• 16 500 / 20 000 m • Air Pressure 70 / 60 hPa, Air Temperature -50 / -90°C
Any season and latitude
Balloon constellation(~20) forming a regional observatory
Light instrumentation (overall suspended weight ~45/50 kg)
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CONCORDIASIPresentation outline
Super Pressure Balloon
Concept
Mission
Technical challenges Balloon Infrastructure and launch
process On board systems Flight monitoring and control Rapid distribution of scientific
data
CONCORDIASIScientific investigatorsMeasurement planLaunch campaignFlight overviewDriftsondesIn situ measurement
1 – Ozone destruction2 – Ozone
depletion/replenishment 3 – Stratospheric Dynamics -
waves
Experiment• Atmospheric sounding
through GPS occultation
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SPB Technical Challenges
Balloon design and operations
Envelope
Strength and endurance Gas-tightness
Operations
• Launch technique compatible with a constellation deployment, must withstand:
• Moderate surface level winds (8-10 kts)• A wide range of ground conditions, from dry and cold winter polar to warm
and moist tropical• A sustained launch rate, 2/3 per week launch rate over several months
• Must not require heavy specific infrastructure
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SPB Technical Challenges
Light mobile means
Launch pad fully set
Inside a “Ractent”
Inflatable launch table
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SPB Technical Challenges
Manual launch technique
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SPB Technical Challenges
On board systems
Reliability Fail safe design Thermal control under extremely variable stratospheric
environmentStringent mass limitation
Photo Holy Troy
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SPB Technical Challenges
Scientific instruments – payload module
Versatile Payload gondolaA standard versatile payload module providing instruments with energy, thermal control, command and data management
It carries up to 3 instruments that must comply with the following overall capabilities:
• Weight ~8 kg • Mean power ~10 w • Daily Mean data rate ~1MByte
Photo J N Valdivia
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SPB Technical Challenges
Flight control, data transfer
Flight control of the flotilla over several months For safety For mission success
6 people on duty 7/73 of them on 24/24 alert through pagers
Scientific Instrument control Hourly data transfer Balloon > Control centers > Internet Daily requests from scientists > Control centers
Global Telecommunication System (WMO) Most of the data is to be transferred promptly to the GTS for
access by the NWP centers.
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SPB Technical Challenges
Flight control / data transfer
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“CCL” Launch Control CenterMcMurdo Station Antarctica
Driftsonde Mission centerMétéo-France, Toulouse F.
Driftsonde control centerNCAR, Boulder Colorado USA
WPC instrument monitoringU. Wyoming, Laramie, Wy.
ROC instrument monitoringPurdue U., W. Lafayette, In.
UCOz instrument monitoringU. Colorado, Boulder Co.
LMDOz and TSENinstruments monitoringCNRS_LMD, Palaiseau, F.
Balloon Control Centers: flight control of the gondola, instrument control and data download
Driftsonde control center:DS payload monitoring and dropsonde data download
WEB based data exchange
Iridium link
“CCT”: Balloon Flight Control CenterToulouse, France
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CONCORDIASIPresentation outline
Super Pressure Balloon
Concept
Mission
Technical challenges Balloon Infrastructure and launch
process On board systems Flight monitoring and control Rapid distribution of scientific
data
CONCORDIASIScientific investigatorsMeasurement planLaunch campaignFlight overviewDriftsondesIn situ measurement
1 – Ozone destruction2 – Ozone
depletion/replenishment 3 – Stratospheric Dynamics -
waves
Experiment• Atmospheric sounding
through GPS occultation
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CONCORDIASIMeasurement plan
MSD PSC
SPBFlight #
Driftsonde fitted with
~50 dropsondes
Meteosensors
OzoneConcentration
PSCaerosols
GPSRadio
Occultation
MSD01 x xMSD02 x xMSD03 x xMSD04 x xMSD05 x xMSD06 x xMSD07 x xMSD08 x xMSD09 x xMSD10 x xMSD11 x xMSD12 x xMSD13 x xPSC14 x x xPSC15 x x xPSC16 x x xPSC17 x x xPSC18 x x xPSC19 x x x
In-situ measurements19 SPB flights
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CONCORDIASIPresentation outline
Super Pressure Balloon
Concept
Mission
Technical challenges Balloon Infrastructure and launch
process On board systems Flight monitoring and control Rapid distribution of scientific
data
CONCORDIASIScientific investigatorsMeasurement planLaunch campaignFlight overviewDriftsondesIn situ measurement
1 – Ozone destruction2 – Ozone
depletion/replenishment 3 – Stratospheric Dynamics -
waves
Experiment• Atmospheric sounding
through GPS occultation
![Page 18: CONCORDIASI - umr-cnrm.fr8 SPB Technical Challenges Balloon design and operations Envelope Strength and endurance Gas-tightness Operations •Launch technique compatible with a constellation](https://reader036.fdocuments.net/reader036/viewer/2022071011/5fc9fd53025ce93d064f61b9/html5/thumbnails/18.jpg)
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CONCORDIASILaunch Campaign
McMurdo unique combination • Accessible during late Winter • Protected from katabatic winds• Well South (~1300 km from Pole)
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CONCORDIASI Launch Campaign
August 20th transfer NZ - McMurdo
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CONCORDIASI Launch Campaign
Preparation
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CONCORDIASI Launch Campaign
Actual launch schedule21 22 23 24 25 26 27 28 29 30 31 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 1 2 3 4 5 6 7
PSCPSCPSCPSCMSDMSDMSDMSDMSDPSCMSDMSDPSCMSDMSDMSDMSDMSDMSD
Launch
Nov.
20 launches over 7 weeks, averaging 3 per week
UnpackingPréparation
September October
Laun
ch p
hase
DismantlingPacking
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CONCORDIASIPresentation outline
Super Pressure Balloon
Concept
Mission
Technical challenges Balloon Infrastructure and launch
process On board systems Flight monitoring and control Rapid distribution of scientific
data
CONCORDIASIScientific investigatorsMeasurement planLaunch campaignFlight overviewDriftsondesIn situ measurement
1 – Ozone destruction2 – Ozone
depletion/replenishment 3 – Stratospheric Dynamics -
waves
Experiment• Atmospheric sounding
through GPS occultation
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CONCORDIASIFlight overview
Flight duration: • overall 1316 days• Average 69 days per flight
Significant loss of measurements (~30% of the potential amount) due to on board loss of communication with the CNES systems (yellow phases)
8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23
PSC15 X
PSC16 XPSC17 X
PSC14 X
MSD01 X
MSD02 X
MSD04 X
MSD05 X
MSD06 X
PSC18 X
MSD07MSD09PSC19 X
MSD10 X
MSD03 XMSD11 X
MSD13MSD12 X
MSD08
Flig
hts Jan.Nov.Sept. Oct. Dec.
Loss of communication with the Payload Supervisory Board
X 3 cut-off for recovery
X 4 cut-off after exhaustion of the solar panels
X 2 cut-off after loss of communication with the Power Management Unit
X 6 cut-off for flight safety
4 balloon bursts
Payload recovered
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CONCORDIASIFlight overview
Trajectories
2010, a stable Austral Winter Polar VortexCourtesy C. Basdevant
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CONCORDIASI Flight overview
3 payloads recovered:
PSC15 et PSC16 near McMurdoPSC17 in Tasmania
Courtesy Arthur River Natl. Natural Park
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CONCORDIASIPresentation outline
Super Pressure Balloon
Concept
Mission
Technical challenges Balloon Infrastructure and launch
process On board systems Flight monitoring and control Rapid distribution of scientific
data
CONCORDIASIScientific investigatorsMeasurement planLaunch campaignFlight overviewDriftsondesIn situ measurement
1 – Ozone destruction2 – Ozone
depletion/replenishment 3 – Stratospheric Dynamics -
waves
Experiment• Atmospheric sounding
through GPS occultation
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CONCORDIASIDriftsondes
DriftsondeReleases dropsondes
that measure from balloon to ground: Pressure Temperature Moisture Wind
50 dropsondes per Driftsonde gondola, dropped on command
Appropriate management of the balloon helium gas
Driftsonde gondola, NCAR
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CONCORDIASI Driftsondes
> 600 dropsondes
Driftsonde operations23 24 25 26 27 28 29 30 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 1
on b
oard
OK
MSD01 47 47MSD02 50 48MSD04 51 49MSD05 53 51MSD06 48 46MSD07 51 46MSD09 50 50MSD10 49 47MSD03 54 53MSD11 54 52MSD13 54 53MSD12 54 54MSD08 47 46
662
642
Drop sondes
Flig
hts
Intensive dropsonde releases ~12 per day for 7 weeks
Sept. Oct. Nov.
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CONCORDIASI Driftsondes
Dropsonde map
Sea-ice limit mid-November
Courtesy NCAR
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CONCORDIASIPresentation outline
Super Pressure Balloon
Concept
Mission
Technical challenges Balloon Infrastructure and launch
process On board systems Flight monitoring and control Rapid distribution of scientific
data
CONCORDIASIScientific investigatorsMeasurement planLaunch campaignFlight overviewDriftsondesIn situ measurement
1 – Ozone destruction2 – Ozone
depletion/replenishment 3 – Stratospheric Dynamics -
waves
Experiment• Atmospheric sounding
through GPS occultation
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CONCORDIASIIn situ measurements-1
Ozone destruction
4 Flights with 3 instruments on board
Particle Counter« WPC »
Thermodynamic Sensors« TSEN »Ozone
photometer
« LMDOz »
Ozone photometer« UCOz »
or++
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CONCORDIASI In situ measurements-1
Ozone destruction
On board 4 flights
Results
Simultaneous measurements from the 3 instruments in the winter vortex at return of daylight over a cumulated durationof 8 weeks
PSC15 and PSC17 flights: Loss of communication with the Payload Supervisory Board (CNES) after 1 weekand 1 month respectively in flight
PSC16 flight: WPC end of life after 3 weeks of intensive use( ~ nominal)
PSC14 flight: WPC early failure after 2 days in flight
8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
PSC15PSC16PSC17PSC14
Sept. Oct.
Flig
hts
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CONCORDIASI In situ measurements-2
Ozone depletion / replenishment
Results
• Cumulated measurement duration 35 weeks• 3 instruments measuring simultaneously during 8 weeks•Good agreement with ozone soundings and data from space borne instruments
•High level of reliability of the photometers•Measurements were interrupted after loss of contact with CNES PSB or Power Management Unit
Ozone photometers on board 6 flights
8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21
PSC15 LMDOzPSC16 UCOzPSC17 UCOzPSC14 LMDOzPSC18 LMDOzPSC19 UCOz
Flig
hts Déc.Sep. Oct. Nov.
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CONCORDIASI In situ measurements-1
Dynamics / waves
TSEN on board each flight
• Position (GPS), every minute• Air Pressure (TSEN), every 30 sec (high accuracy Paroscientific)• Air Temperature (TSEN), every 30 sec (micro-thermistor)
ResultsData collected over ~900 days Measurements were interrupted after loss of contact with CNES PSB or Power Management Unit
8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23
PSC15PSC16PSC17PSC14MSD01MSD02MSD04MSD05MSD06PSC18MSD07MSD09PSC19MSD10MSD03MSD11MSD13MSD12MSD08
Flig
hts Jan.Nov.Sept. Oct. Dec.
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CONCORDIASIPresentation outline
Super Pressure Balloon
Concept
Mission
Technical challenges Balloon Infrastructure and launch
process On board systems Flight monitoring and control Rapid distribution of scientific
data
CONCORDIASIScientific investigatorsMeasurement planLaunch campaignFlight overviewDriftsondesIn situ measurement
1 – Ozone destruction2 – Ozone
depletion/replenishment 3 – Stratospheric Dynamics -
waves
Experiment• Atmospheric sounding
through GPS occultation
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CONCORDIASIExperiment
Atmosphere sounding through GPS Occultation
2 “PSC” flights partly dedicated to experimental atmospheric sounding through GPS occultation from stratospheric balloons.
“ROC” instrument includes:One or two dual band
GPS receiversOn board data processing
for minimization ofdownlink data flow
ROC onboard together withOzone photometer
and TSEN
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CONCORDIASI Experiment
Atmosphere sounding through GPS Occultation
Results
Measurements over 15 weeks
Measurements have been interrupted after loss of contact with CNES PSB or Power Management Unit
29 30 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30
PSC18 ROC 1PSC19 ROC 2
Nov.
Flig
hts Oct.
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CONCORDIASIResult overview
Technical
Excellent reliability of the scientific instruments• All 13 Driftsonde gondolas performed very well with a 95% success rate• Out of 29 other instruments on board just one unit failed prematurely
Overall very good performance of the flight systems, control centers and flight operations
• Mature Iridium based flight control and data transfer system• Efficient renewable power system• Anomaly on on-board CNES systems reduced the potential amount of in-
situ data collection by 30% , investigation by CNES still in progress. Impact on scientific mission achievement limited, thanks to an
overall high redundancy levelAnomaly on the balloons. 3 balloons did burst unexpectedly
after months in flight while drifting well inside their design limits
• Investigation by CNES in progress, apparent progressive damage ?• Did not impact significantly the scientific mission
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CONCORDIASIAcknowledgements
Excellent international cooperation With the scientific teams for the long validation phase Support at McMurdo station Flight Operations by CNES and Météo-France teams in Toulouse, and
NCAR in Boulder The result of a long standing effort to expand the scientific capabilities
of long duration flights by CNES balloon, flight systems and operations teams Industry teams Zodiac, ELTA, Sogeti, R-Tech, Atelier Image, and others Science teams bringing unswerving motivation and meteorology expertise
The outcome of a long standing effort to develop a consistent and efficient Balloon-Driftsonde system between CNES and NCAR
http://www.cnrm.meteo.fr/concordiasi/http://www.lmd.polytechnique.fr/VORCORE/McMurdo.htm
Author: Philippe Cocquerez, CNES Toulouse Space Center, DCT/BL/PR
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CONCORDIASI
B.U.S.
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CONCORDIA-IASI
A French-US initiative for climate / meteorology over Antarctica and at global scale
Improve the use of space-borneatmospheric sounders over polar regions, in particular“IASI" on board MetOp
Benefit from the continentalFrench-Italian station“CONCORDIA”
on board MetOp
Concordia Station
IASI Sounder
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CONCORDIASIMotivations
Main goals:
To improve the assimilation of satellite data over the southern polar region, and more generally over ice regions In particular for the new IASI sounder And thus to improve weather predictions.
To improve understanding of stratospheric ozone Through examination of the interaction of ozone at flight level and
stratospheric clouds Together with the improved characterization of the polar vortex.
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CONCORDIASIMotivations
Main goals:
To provide recommendations on the design of the global observing system over the southern polar region By determining the extent to which additional observations over Antarctica
can improve the prediction of high impact weather over lower latitudes.
To advance understanding of the Earth system By examining the two-way interactions between the climates of Antarctica
and lower latitudes.
Labeled « Thorpex » by the World Meteorological Organization
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CONCORDIASIPresentation outline
Super Pressure Balloon
Concept
Mission
Technical challenges Balloon Infrastructure and launch
process On board systems Flight monitoring and control Rapid distribution of scientific
data
CONCORDIASIScientific investigatorsMeasurement planLaunch campaignFlight overviewDriftsondesIn situ measurement
1 – Ozone destruction2 – Ozone
depletion/replenishment 3 – Stratospheric Dynamics -
waves
Experiment• Atmospheric sounding
through GPS occultation
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CONCORDIASIScientific Investigators
Principal Investigator: – Météo-France , (CNRM-GAME Toulouse, F), Florence Rabier
Investigator / Experimenter (on board SPB)– CNRS / LMD (Palaiseau, F)– National Center for Atmospheric Research (Colorado, USA)– University of Wyoming (Laramie, USA)– University of Colorado in Boulder (USA)– Purdue University (West Lafayette, Indiana, USA)
Investigator / Experimenter (Concordia and Dumont d’Urville)– CNRS / LGGE (Grenoble, F)– Météo-france
Investigators– ECMWF– Met Office UK
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CONCORDIASIAgency commitments
National Science Foundation (USA)• US instrument development and production• US scientists for field experiment • Logistics, infrastructure and life support at McMurdo Station.
CNES• French scientific experiments• Development and production of all flight and ground hardware • Field experiment and flight control operations• Overall technical management of the experiment
Institut Polaire Français IPEV• Support to promote Concordiasi as an international program in Antarctica• Measurements from Concordia and Dumont d’Urville
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CONCORDIASIMeasurement plan
Driftsonde payload (13 “MSD” flights )
Perform 600 soundings of the atmosphere beneath the balloon over the Antarctic region, at times / situations chosen by météo-France
~70% during overpasses by IASI and/ or AIRS space borne instruments~30% “Targeting” over sensitive areas
« Driftsonde » gondola developed by NCAR A driftsonde releases on command up to 50 “Dropsondes” which measure from
balloon to ground:– Pressure– Temperature– Moisture– Wind
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CONCORDIASI Measurement plan
In situ Measurements
1 – Ozone destruction (4 PSC flights), Links among stratospheric chemistry, dynamics and cloud microphysicsKey period : early Sept. to mid-Oct.
• Detection and quantification of PSC related aerosols : « WPC », U. Wyoming• Ozone concentration : « LMDOz », CNRS-LMD or « UCOz », UC Boulder• Air temperature : « TSEN », CNRS-LMD
2 – Ozone depletion / replenishment(6 PSC flights)Key period : early September to late December • Ozone concentration : LMDOz or UCOz• Air temperature and pressure, trajectory : TSEN
3 – Meso-scale stratospheric dynamics-waves (13 MSD and 6 PSC flights)Key period : as long as possibleSpace and time high resolution measurements of pressure and position • Pressure variations : TSEN• Balloon position : GPS on board CNES systems
GPS occultation experiment (2 PSC flights)
• Dual band GPS receivers « ROC », U. Purdue
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CONCORDIASI Measurement plan
Ozone soundings at overpass of the SPB PSC flightsFor calibration of the ozone photometers
From the following stations:• Amundsen–Scott, USA• Belgrano, Sp.-Arg. • Davis, Aus.• Dumont d’Urville, Fr.• McMurdo, USA• Neumayer, Ger.• Siowa, Jap.
Augmented atmosphere observation plan at
• Concordia, LGGE / IPEV-PNRA• Rothera, UK
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CONCORDIASIResults overview
Science
Collection of huge amounts of data at the right time and the right place, often unprecedented, will produce very valuable scientific outcomes
Scientific exploitation in progress• Data validation• Post flight calibration on several instruments after recovery• Analysis/modeling
Second scientific workshop at NCAR in Boulder October 2011
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CONCORDIASIStep back to the future
Pre - CONCORDIASI took place early 2010, 3 flights, 3 months each
α As a successful preparation for CONCORDIASI
Ω As an anticipation of STRATEOLE II, scheduled over 2016-2018Study of the Tropical Upper Troposphere Lower Stratosphere