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AMERICANMETEOROLOGICALSOCIETY
Bulletin of the American Meteorological Society
EARLY ONLINE RELEASEThis is a preliminary PDF of the author-producedmanuscript that has been peer-reviewed and accepted for publication. Since it is being postedso soon after acceptance, it has not yet beencopyedited, formatted, or processed by AMSPublications. This preliminary version of the manuscript may be downloaded, distributed, andcited, but please be aware that there will be visualdifferences and possibly some content differences between this version and the final published version.
The DOI for this manuscript is doi: 10.1175/BAMS-D-12-00075.1
The final published version of this manuscript will replacethe preliminary version at the above DOI once it is available.
© 2013 American Meteorological Society
1
Driftsondes: Providing In-Situ Long-Duration Dropsonde Observations over Remote Regions 1
2
Stephen A. Cohn1, Terry Hock1, Philippe Cocquerez2, Junhong Wang1, Florence Rabier3, David 3
Parsons4, Patrick Harr5, Chun-Chieh Wu6, Philippe Drobinski7, Fatima Karbou3, Stéphanie 4
Vénel2, André Vargas2, Nadia Fourrié3, Nathalie Saint-Ramond3, Vincent Guidard3, Alexis 5
Doerenbecher3, Huang-Hsiung Hsu8, Po-Hsiung Lin6, Ming-Dah Chou9, Jean-Luc Redelsperger10, 6
Charlie Martin1, Jack Fox1,11, Nick Potts1, Kathryn Young1, and Hal Cole1 7
8
1National Center for Atmospheric Research, Boulder, CO, USA 9
2Centre National d’Etudes Spatiales, Toulouse, France 10
3CNRM-GAME, Météo-France and CNRS, Toulouse, France 11
4University of Oklahoma, Norman, OK, USA 12
5Naval Postgraduate School, Monterey, California, USA 13
6National Taiwan University, Taipei, Taiwan 14
7Ecole Polytechnique/CNRS, Palaiseau, France 15
8Research Center for Environmental Change, Academia Sinica, Taipei, Taiwan 16
9National Central University, Taiwan 17
10Laboratoire de Physique des Océans, CNRS, IFREMER, IRD, UBO, France 18
11now at Advanced Radar Corporation, Boulder, CO, USA 19
20
2
Corresponding author: Stephen A. Cohn, National Center for Atmospheric Research 21
PO Box 3000, Boulder, CO 80307-3000 USA 22
Email [email protected] 23
For submission to the Bulletin of the American Meteorological Society 24
November 2012 25
Revised: February 2013 26
3
Abstract 27
Constellations of Driftsonde Systems, gondolas floating in the stratosphere and able to release 28
dropsondes upon command, have so far been used in three major field experiments from 2006 29
through 2010. With them, high-quality, high-resolution, in-situ atmospheric profiles were made 30
over extended periods in regions that are otherwise very difficult to observe. The 31
measurements have unique value for verifying and evaluating numerical weather prediction 32
models and global data assimilation systems; they can be a valuable resource to validate data 33
from remote sensing instruments, especially on satellites, but also airborne or ground based 34
remote sensors. These applications for models and remote sensors result in a powerful 35
combination for improving data assimilation systems. Driftsondes also can support process 36
studies in otherwise difficult locations, for example to study factors that control the 37
development or decay of a tropical disturbance, or to investigate the lower boundary layer over 38
the interior Antarctic continent. The Driftsonde System is now a mature and robust observing 39
system that can be combined with flight-level data to conduct multidisciplinary research at 40
heights well above that reached by current research aircraft. In this article we describe the 41
development and capabilities of the Driftsonde System, the exemplary science resulting from its 42
use to date, and some future applications. 43
44
4
Capsule: 45
A long-duration balloon-borne dropsonde platform brings innovative technology for multi-46
disciplinary science to hard-to-reach parts of the globe from heights unobtainable by research 47
aircraft. 48
5
1. Introduction 49
High quality in-situ measurements from radiosondes and dropsondes are the gold 50
standard for vertical profiles of fundamental atmospheric measurements such as wind, 51
temperature, and relative humidity. Satellite-borne remote sensors provide much-needed 52
global, long-term coverage, but do not match the ability of sondes to capture sharp transitions 53
and fine vertical structure, and have significant performance limitations (e.g., inability of 54
infrared sounders to penetrate clouds, poor accuracy in the boundary layer). Sondes are also a 55
trusted means to calibrate and validate remote sensors. However, it is challenging to launch 56
radiosondes from remote locations such as the ocean surface or the interior of Antarctica. 57
Aircraft release dropsondes above such locations, but are limited by the range and endurance 58
of the aircraft. The Driftsonde System fills an important gap in our ability to use sondes to 59
measure atmospheric profiles in remote locations. Although its creation was motivated by the 60
THORPEX (The Observing System Research and Predictability Experiment, e.g. Shapiro and 61
Thorpe 2004) to optimize the global observing system, it has contributed to varied 62
investigations ranging from understanding the development of tropical cyclones to validation of 63
satellite retrievals in Antarctica. 64
The Driftsonde is a unique, balloon-borne instrument that releases dropsondes to 65
provide high resolution in-situ profiles of atmospheric temperature, humidity, pressure, and 66
winds from the lower stratosphere down to the surface. It is ideal for applications over oceans 67
and remote polar and continental regions, filling critical gaps in data coverage where the 68
release of surface-based radiosondes is not possible. Figure 1 shows the Driftsonde System 69
6
concept in which a stratospheric balloon carries the Driftsonde gondola with a large number of 70
Miniature In-situ Sonde Technology (MIST) dropsondes for days to months. The balloon drifts 71
with the wind and sondes are released upon command. They parachute to the ground 72
providing high vertical resolution profiles. Data from each sonde are transmitted back to the 73
gondola, and from there to the ground via an Iridium satellite link. Commands from the ground 74
are also relayed to the gondola via satellite link. Data can be quality-checked in near real-time 75
and sent to the Global Telecommunications System (GTS), making it available for operational 76
and research uses such as Numerical Weather Prediction (NWP) models and to direct in-the-77
field experimental planning. The Driftsonde concept of launching dropsondes from balloons 78
was initially developed in the 1970s for the Global Atmospheric Research Program (GARP e.g., 79
Lally and Passi 1976). Although test flights were successfully completed, the instrument was not 80
used for GARP. The concept was revived for THORPEX in a discussion at the National Center for 81
Atmospheric Research (NCAR) between Melvin Shapiro, Vin Lally, Terry Hock, and Hal Cole, with 82
subsequent simulations by Rolf Langland (Naval Postgraduate School) confirming its potential 83
reach. 84
The Driftsonde System consists of the flight train shown in Figure 2, ground control 85
software which is web based, and ground control servers and associated hardware located at 86
NCAR in Boulder, Colorado. Web based software adds flexibility, so that an experiment 87
operations center can be located worldwide, or may rotate through several locations to support 88
the continuous (24-h, 7-day) nature of balloon flight operations. The latest version of the 89
gondola structure (Figure 3), made of insulating foam, contains up to 54 MIST dropsondes, a 90
custom electronics motherboard which acts as the brain of the system, lithium batteries to 91
7
power the gondola for the expected flight duration, radio equipment to communicate both 92
with a released dropsonde and with Iridium satellites, and electric heaters to maintain the 93
gondola electronics and batteries at an operational temperature. The heaters are powered by 94
solar panels mounted outside the gondola. Heating the sonde electronics and batteries before 95
they are released from the gondola ensures the sensors will operate normally. Early Driftsonde 96
tests were done with several ballooning partners1. Subsequent deployments have been a close 97
collaboration between NCAR and the French Centre National d’Etudes Spatiales (CNES) with 98
NCAR developing the Driftsonde measurement capability (gondola, MIST sondes, 99
communications, data quality, etc.), and CNES having responsibility for all ballooning 100
development and flight operations. 101
Characteristics of the Driftsonde’s MIST dropsondes are shown in Table 1. They are 102
physically smaller and lighter than current aircraft dropsondes but both use the Vaisala RSS921 103
sensor module, with the same pressure, temperature, and humidity sensors as the well 104
documented RS92-SGP radiosonde (Vaisala, 2013). Each MIST dropsonde undergoes a 105
calibration verification step at NCAR. While the MIST dropsondes make similar measurements 106
to aircraft dropsondes, the two platforms – Driftsonde gondola and aircraft - have notable 107
differences. Capabilities of the stratospheric balloons used to lift Driftsonde are central to its 108
strengths and limitations. Aircraft are maneuverable, but can remain aloft for only a few hours. 109
They also can precisely target specific locations. The Driftsonde is not maneuverable, but can 110
1 Before and between field projects, we received assistance with ballooning tests from Terry Deshler and the
University of Wyoming, Tim Lachenmeier and Near Space Corporation, Inc., and the NASA Columbia Scientific
Ballooning Facility.
8
remain aloft for several months. Sondes are released from much higher altitudes than most 111
aircraft (Figure 4), and multiple Driftsondes can be in flight simultaneously. In the just 112
completed Concordiasi experiment, a constellation of 13 Driftsondes were aloft simultaneously 113
for about two months, with drops controlled from the ground in McMurdo Station, Antarctica, 114
Toulouse, France, and Boulder, Colorado. In general, because stratospheric balloons drift with 115
the wind and have long duration, Driftsonde data can provide synoptic-scale or finer 116
observations with wide-ranging geographical coverage that would be difficult to obtain with 117
research aircraft. On the other hand, precise targeting of drops is limited by the accuracy of 118
balloon trajectory forecasts. 119
2. Field Experiments and Science Applications 120
As the Driftsonde System was developed (Figure 5), it was deployed in three field 121
experiments associated with THORPEX activities (Table 2). Each revealed and led to needed 122
improvements, and from these experiments we also learned better how to take advantage of 123
the system’s strengths for varied science applications. Details of the Driftsonde System 124
performance and scientific applications in each experiment are presented in the following 125
sections. 126
a. Driftsonde observations during the African Monsoon Multidisciplinary Analyses 127
The first field project experience with Driftsonde was in the African Monsoon 128
Multidisciplinary Analyses (AMMA) project2, both as a rigorous field test and for its scientific 129
2 AMMA, based on a French initiative, was organized by an international scientific group and is currently funded by
a large number of agencies, especially from France, UK, US and Africa. It has been the beneficiary of a major
9
value. AMMA was organized to advance understanding of the West African Monsoon system 130
and to improve predictions of its variability and the associated wide range of societal impacts. It 131
is a major international program led by France, but involving agencies and scientists located in 132
the United Kingdom, Germany, the United States, and other countries across Africa and Europe. 133
The Driftsonde deployment supported AMMA’s research focus on high-impact weather and 134
was undertaken through a collaboration between AMMA and THORPEX. The program is 135
summarized in Redelsperger et al. (2006), with the Driftsonde observing strategy described in 136
Rabier et al. (2008). 137
The AMMA measurement strategy included long-term observations from 2002 through 138
2010 to investigate the inter-annual variability of the West African Monsoon. Within this period 139
was an Extended Observing Period (EOP) from 2005-2007 to document the annual cycle, and 140
four Special Observing Periods (SOPs) during 2006 to provide specific observations of physical 141
processes and of weather systems. The Driftsonde operations took place during the 4th SOP 142
covering the late monsoon period in August and September 2006. 143
The Driftsonde deployment was considered a THORPEX Observing System Test (e.g., 144
Shapiro and Thorpe 2004). Thus, a large component of Driftsonde operations concentrated on 145
engineering tests, including the first major test of NCAR’s new smaller and lighter dropsonde 146
called MIST, which at 175 g was less than half the weight of the previous dropsondes and was 147
financial contribution from the European Community's Sixth Framework Research Programme. Detailed
information on scientific coordination and funding is available on the AMMA International web site
http://www.amma-international.org.
10
developed specifically for use in the Driftsonde. Miniaturization of the dropsonde was 148
necessary for ballooning where weight is more critical than for aircraft deployments. For 149
AMMA, the Driftsonde gondola held 49 MIST dropsondes. The AMMA deployment was the first 150
scientific use of the new CNES 12-m super pressure balloons, the new NCAR gondolas and the 151
MIST dropsondes. 152
Eight Driftsondes were launched from Zinder, Niger, and floated at about 20 km as they 153
drifted eastward reaching the Atlantic Ocean. The location was chosen to allow investigators to 154
study both African Easterly Waves over central and western Africa and the potential 155
intensification of these waves into tropical disturbances or even hurricanes over the subtropical 156
Atlantic. Flight trajectories and the dropsonde locations are shown in Fig. 6. The dropsondes 157
were able to sample both the Saharan Air Layer that is often advected over the tropical Atlantic 158
and precursor environments, and the near-storm environments associated with 2006 tropical 159
storm Florence and hurricanes Gordon and Helen. The first balloon was launched on 28 August 160
2006 and the termination of the final balloon over the central subtropical Atlantic occurred on 161
22 September. Two balloons had mission durations in excess of 8 days. Sondes were typically 162
deployed near 0000 and 1200 UTC as well as on demand for promising weather conditions. For 163
further details on the Driftsonde operations during AMMA, a description of the challenges 164
associated with balloon and dropsonde design and preliminary scientific results, refer to the 165
overview of the deployment presented in Drobinski et al. (2006) and Drobinski et al. (2012a). 166
Much was learned about the system’s operation and performance as 124 sondes were 167
successfully deployed from the 8 Driftsonde gondolas. While there was one premature failure 168
11
of a stratospheric balloon and lessons learned about Driftsonde launch procedures, most 169
engineering challenges highlighted the need to improve aspects of the Driftsonde gondola 170
design and usability of system software. There were many cases where sondes failed to launch, 171
as well as periods of lost communication between the ground control station and the gondola. 172
Another significant conclusion was the need to redesign the MIST sonde to include a pressure 173
sensor. A pressure sensor was not included in the AMMA version of the MIST sonde because of 174
the incorrect assumption that the pressure for the dropsonde profile could be obtained from 175
knowledge of the pressure and GPS altitude at launch and the hydrostatic equation. However, 176
the flight level pressure sensor on the gondolas did not have sufficient accuracy, so small errors 177
in the initial pressure were magnified by the downward integration of the hydrostatic equation. 178
A success of AMMA was the demonstrated ability to target measurements with 179
Driftsondes launched 4-5 days before the sampling window. The successful sampling of storms 180
was due to the accuracy of the upper-level winds predicted from operational NWP models, the 181
quasi-non-divergent nature of the flow at 20 km, and successful tropical storm genesis 182
forecasts by the AMMA team through combining experimental and operation products for 183
storm genesis. 184
Despite technical challenges, AMMA demonstrated the scientific value of Driftsonde, in 185
particular to evaluate operational model performance and identify specific areas for model 186
improvement. Drobinski et al. (2012b) use Driftsonde and other data to evaluate performance 187
of the ECMWF Integrated Forecast System (IFS) and the two versions of the Météo-France 188
ARPEGE operational forecast system through comparison of the dropsonde observations and 189
12
the model analysis and prediction. The concept was to improve performance in key regions and 190
different flow regimes using the special dropsonde observations to supplement the assessment 191
procedure employed by the operational centers. This technique was extended to evaluate the 192
impacts of recent upgrades in model physics and assimilation techniques. 193
The findings from Drobinski et al. (2012b) include that these models well represent the 194
complex vertical structure of humidity associated with the Saharan Air Layer (Fig. 7a). However, 195
the comparison identified temperature errors of several degrees C in both modeling systems 196
near the base of the Saharan Air Layer (Fig. 7b). The relatively large errors are likely because of 197
the lack of dust and the associated radiative impacts within NWP models. This result suggests 198
shortcomings in the assimilation system, perhaps due to the vertical resolution of the satellite 199
data, and argues for the inclusion of aerosols and their radiative effects in NWP models. In this 200
case, static stability errors in the vicinity of the Saharan dust could, in turn, impact the 201
likelihood, intensity and structure of convection. Considerable debate currently exists in 202
determining and explaining the potential impacts of the Saharan Air Layer on tropical cyclones 203
(e.g., see Braun 2010 and references therein). It was also found that within the analyses, the 204
zonal and meridional winds in the Saharan Air Layer cases have significant errors (Figs. 7c and 205
d). The Driftsonde observations were also valuable as “ground-truth” in data impact and data 206
assimilation experiments (Drobinski et al, 2012b). 207
b. Driftsonde observations during the THORPEX-Pacific Asian Regional Campaign 208
The Driftsonde experience in AMMA was a success both in identifying technical issues 209
which needed attention after the campaign and collecting scientifically valuable observations. 210
13
Prior to the next large field use in the THORPEX-Pacific Asian Regional Campaign (T-PARC)3 in 211
2008, many parts of the system were upgraded. In particular a pressure measurement was 212
added to the MIST sonde, robustness of the satellite communication link was improved, and 213
reliability of the sonde separation from the gondola when a drop is commanded was also 214
improved. 215
As a multi-national field campaign and research initiative, T-PARC addressed the 216
shorter-range dynamics and forecast skill of one region (eastern Asian and the western North 217
Pacific) and its downstream impact on the medium-range dynamics and forecast skill of another 218
region (eastern North Pacific and North America). High-impact weather events over the regions 219
examined in T-PARC have strong dynamical links downstream. For example, persistent deep 220
tropical convection or the extratropical transition of tropical cyclones can trigger downstream 221
responses over the eastern North Pacific, North America, and beyond via upper-tropospheric 222
wave packets on the primary midlatitude waveguides (Anwender et al. 2008, Harr et al. 2008). 223
Then, wave packets can be invigorated by subsequent downstream cyclogenesis events that are 224
often associated with reduced predictability. High-impact weather events over North America 225
driven by these processes can include intense extratropical cyclones, floods, severe weather 226
and hot, dry winds that increase the risk of wildfires and the severity of droughts. While T-PARC 227
objectives encompassed mesoscale and synoptic-scale processes associated with tropical 228
cyclones over the western North Pacific and eastern Asia, they also addressed medium-range 229
forecast skill associated with downstream impacts across the North Pacific and beyond. 230
3 T-PARC was supported financially by Germany, Canada, Japan, Australia, France, Korea, Taiwan, the U.K., the
European Centre for Medium-Range Weather Forecasts, and the United States.
14
Dropsondes were an important contribution to T-PARC. In addition to use of Driftsonde, 231
four aircraft from three countries [U.S.: USAF WC-130J and NRL P-3, Taiwan: DOTSTAR Astra 232
(Wu et al. 2005, 2007a), and Germany: DLR Falcon] were used to take special observations. The 233
collaborative program required an experimental design that covered a very wide geographic 234
range to address three primary components: (1) A tropical measurement strategy examined 235
circulations of the tropical western North Pacific monsoon environment as they related to 236
enhanced and reduced periods of widespread deep convection, tropical cyclone formation, 237
tropical cyclone intensification, and tropical cyclone structure change; (2) A measurement 238
strategy for the extratropical transition and its downstream impacts followed the poleward 239
movement of a decaying tropical cyclone and the intense cyclogenesis that results from its 240
interaction with the midlatitude circulation; and (3) A targeted observation strategy focused on 241
regions in which extra observations may reduce numerical forecast error growth (Wu et al. 242
2007b, 2009, Harnisch and Weissmann 2010, Reynolds et al. 2010, Weissmann et al. 2010, Chou 243
et al. 2011). In T-PARC, the targeted observations were aimed at reducing errors associated 244
with tropical cyclone track forecasts, which included whether a tropical cyclone would recurve, 245
the longitude of recurvature, and the orientation and speed along the track following 246
recurvature. 247
To accomplish the primary objectives of T-PARC, a complete tropical-to-extratropical 248
measurement strategy was necessary. For example, predictability associated with extratropical 249
transition depends on the intensity and structure of the tropical cyclone, where and when the 250
tropical cyclone arrives in the midlatitude westerlies, the characteristics of the midlatitude 251
15
waveguide that impact the extratropical transition-related cyclogenesis, and the downstream 252
propagation and evolution of the wave packets. 253
The motivation for deployment of Driftsondes in T-PARC was to provide measurements 254
over data sparse regions of the tropical central Pacific. The data from the Driftsonde 255
complemented satellite observations and provided calibration and validation data for new 256
satellite-based observations (Hawkins and Velden 2011) and global reanalysis products (Wang 257
et al. 2010). During T-PARC, 16 Driftsondes were launched from the southern end of the Big 258
Island of Hawaii between 15 August and 30 September 2008. Thirteen of the Driftsondes 259
traveled at an altitude of about 30 km for up to five days to reach the western North Pacific and 260
the primary T-PARC observation region (Figure 8). Throughout T-PARC, 254 dropsondes were 261
deployed from the Driftsondes. The location and timing of the dropsonde deployments were 262
coordinated from the T-PARC operations center at the Naval Postgraduate School in Monterey, 263
CA, taking advantage of the now web-based Driftsonde control and display software. During 264
each balloon flight, data were relayed to the T-PARC operations center, quality controlled, and 265
transmitted to the GTS for use at operational weather centers. 266
As an example of Driftsonde use during T-PARC, the fourth Driftsonde was launched on 267
24 August 2008 and on 29 August it reached a tropical disturbance that was being investigated 268
by the T-PARC aircraft (Figure 9). While the Driftsonde was over-flying the tropical disturbance 269
in the lower stratosphere two aircraft were deploying dropsondes from their respective flight-270
level altitudes. Seven dropsondes were deployed from the Driftsonde and provided 271
16
measurements of two upper-tropospheric cyclonic systems that were preventing the 272
development of the tropical disturbance. 273
Driftsondes in T-PARC were flown with zero-pressure balloons. These were designed to 274
float much higher than the super-pressure balloons used for AMMA (and later in Concordiasi), 275
but also had a shorter flight lifetime. Because of light winds and a flaw in the ballooning 276
technique several flights failed to advect far enough westward to enter the most interesting 277
measurement region. However, overall, data obtained from dropsondes released from the 278
Driftsondes provided valuable measurements of persistent deep convection with special 279
emphasis on the detailed vertical structure, impacts of vertical wind shear, and upper-level 280
divergent outflow. Because of the Driftsonde launch location and trajectories, data were 281
instrumental in monitoring tropical cloud clusters that migrated over the data-sparse region of 282
the tropical central Pacific until the clusters reached the region of T-PARC aircraft operations. 283
c. Driftsonde observations during the Concordiasi Field Experiment 284
The third major Driftsonde deployment was in 2010 for the Concordiasi field 285
experiment4 (Rabier et al, 2010 and 2013), a multi-disciplinary effort jointly conducted by 286
several groups in France and the United States to study the lower stratosphere and 287
4 Concordiasi was organized by an international scientific group and supported by the following agencies: Météo-
France, CNES, IPEV, PNRA, CNRS/INSU, NSF, NCAR, Concordia consortium, University of Wyoming, Purdue
University, and the University of Colorado. ECMWF also contributed to the project through computer resources
and support, and scientific expertise. The two operational polar agencies PNRA and IPEV are thanked for their
support at Concordia station.
17
troposphere above Antarctica. Concordiasi was one of the cluster of THORPEX projects 288
associated with the International Polar Year (e.g., Renfrew et al. 2008, Hanesiak et al. 2010, 289
Kristjánsson et al. 2011). The primary focus of Concordiasi was to validate the use of satellite 290
observations and to document which observing systems are most relevant for numerical 291
weather prediction over the polar areas. Concordiasi field experiments took place in Austral 292
springs 2008, 2009, and 2010, including surface measurements and radiosoundings at the 293
Concordia Antarctica station at Dome C, and radiosoundings at the Dumont d'Urville and 294
Rothera sites on Antarctica. In 2010 Driftsonde was part of an innovative constellation of 295
balloons that provided a unique set of measurements spanning a large spatial extent (both 296
horizontal and vertical) and time. The balloons drifted for several months in the lower 297
stratosphere around 18 km, circling over Antarctica in the polar vortex. The balloon flotilla 298
formed a regional observatory of the atmosphere. As in the earlier Driftsonde experiments, 299
hundreds of soundings were performed on command. The launch campaign took place from 300
the U.S. McMurdo Station, located at 78° south latitude. Nineteen balloons were launched 301
between 8 September and 26 October 2010. The mean flight duration was 69 days, while the 302
longest flight lasted 95 days. Thirteen balloons carried a Driftsonde, and six carried other 303
instruments for Concordiasi. The long flight duration of the super pressure balloons used for 304
Concordiasi, months rather than about a week for the previous Driftsonde use, was critical to 305
enable the project’s science. 306
To prepare for Concordiasi, the Driftsonde System was modified for the much longer 307
duration flights and challenging range of thermal conditions it would encounter. Early in this 308
high latitude project the gondolas were in total darkness, and later in the project they 309
18
transitioned to full sunlight. The software was also enhanced to allow for drops at pre-310
scheduled times. Overall, the 13 Driftsonde gondolas returned 644 high-quality profiles, with 311
only 14 failed drops. This is a much higher success rate than in either AMMA or T-PARC, and 312
resulted in an excellent spatial distribution of observations both over the Antarctic continent 313
and the surrounding ocean. Figure 10 shows the comprehensive coverage and distribution of 314
drop locations over the full experiment, as well as an example of the coverage of the 315
constellation on a single day. 316
Many dropsondes were released to coincide with Driftsonde overpasses of Concordia 317
station, allowing comparison of dropsonde and radiosonde profiles, and also to coincide with 318
overpasses of the MetOp satellite, allowing comparison with data from the Infrared 319
Atmospheric Sounding Interferometer (IASI). IASI is an advanced infrared sounder which has a 320
large impact in NWP systems in general. However, there are some difficulties in its use over 321
polar areas because the extremely cold polar environment makes it more difficult to extract 322
temperature information from infra-red spectra and makes it difficult to detect cloud 323
properties. As a consequence, IASI is currently under-utilized over Antarctica. 324
A number of important results have already come from the 2010 Concordiasi dataset, as 325
described in the Concordiasi workshop report (Rabier et al, 2013). Wang et al. (2013) compare 326
sonde profiles with satellite retrievals, using the NOAA PROducts Validation System (NPROVS) 327
to match Concordiasi dropsonde and radiosonde profiles with profiles from several satellite 328
products. A comparison of temperature profiles shows a cold bias present in all satellite data. 329
The cold bias has larger magnitude relative to the dropsonde data than the radiosonde for all 330
19
satellite products except the COSMIC (The Constellation Observing System for Meteorology, 331
Ionosphere, and Climate) (Fig. 11). The difference between the radiosonde and dropsonde bias 332
can be traced to a larger cold bias over the Antarctic continent than over the coast and ocean 333
since all radiosonde stations but two are located along the coast (Fig. 10a). The source of this 334
bias remains a topic of investigation. Aside from the bias, and an inability to resolve detailed 335
thermodynamic structures near the surface and tropopause, the satellite retrievals reproduce 336
the temperature profiles reasonably well. 337
In addition to temperature and humidity profiles, cloud properties such as cloud top 338
pressure and cloud effective emissivity (emissivity of an equivalent single layer cloud) can be 339
retrieved from IASI measurements. These retrievals are highly dependent on the quality of 340
temperature and humidity profiles. As reported in Rabier et al. (2013), detection of cloud 341
properties can be improved by using an accurate atmospheric profile provided by the 342
Concordiasi dropsondes rather than the atmospheric model. 343
Another result from this dataset comes from the use of Concordiasi Driftsonde 344
observations in real-time at NWP centers. As noted in Rabier et al (2013), large systematic 345
differences exist between various NWP analyses and forecasts for temperature over Antarctica, 346
and for winds on the surrounding oceans. Comparison between short-range forecasts and the 347
Concordiasi dropsonde data show that models poorly represent near-surface temperature over 348
the Antarctic high terrain. The strong thermal inversions are challenging because numerical 349
models need very good representations of both turbulent exchange processes and snow 350
processes to simulate this extreme atmospheric behavior. The difference between the 351
20
dropsonde and the model temperatures at the lowest model level is presented in Figure 12 for 352
the French global model. The model is too warm over the plateau in Antarctica, and it is too 353
cold over the surrounding sea-ice. 354
The impact of dropsondes on NWP models has also been studied with data denial 355
experiments and advanced data impact diagnostics. Dropsondes have a positive impact on the 356
forecast performance in different models, with an impact of the same order of magnitude as 357
that of radiosondes. Rabier et al (2013) report that the average error reduction per observation 358
is much larger for dropsondes than for satellite data, and that dropsonde observations have 359
greater impact when they are closer to the pole. In Figure 13, the impact of dropsonde 360
temperature and wind profiles is illustrated at high levels (pressure less than 400 hPa) and low 361
levels (pressure greater than 400 hPa), together with the number of observations. Overall, 362
temperature information contributes most at low levels, and wind information contributes 363
more at high levels. However on a per-observation basis both wind and temperature have 364
larger impact at low levels, where there are very few other observations. 365
These results from Driftsonde data in Concordiasi provide insight into improvements to 366
the global observing system that must be achieved to improve NWP over the polar areas. This is 367
important not only to improve forecast performance but also for producing more accurate re-368
analyses of the atmosphere to document climate change. 369
3. Conclusion 370
Thanks to the Driftsonde System, in-situ measurements were obtained in parts of the 371
world which are not accessible by any other means. This has provided invaluable information 372
21
about model strengths and weaknesses, and about which observations will be needed in the 373
future to monitor the climate, especially in polar areas. The excellent technical success 374
achieved during Concordiasi demonstrates that Driftsonde is now a mature, reliable, and 375
productive observing system. Its strengths include the ability to reach difficult parts of the 376
globe, to collect highly accurate, in-situ dropsonde profiles, to reliably release up to 54 377
dropsondes per system from the lower stratosphere, and to be deployed as a constellation with 378
many Driftsondes flying simultaneously. 379
Like aircraft dropsonde systems, field experiments using Driftsondes involve significant 380
cost and require much advance planning. It can take months to understand likely flight paths 381
and obtain permissions to overfly many countries. If a balloon drifts near a region where 382
overflight permissions have not been granted, it must be cut down. The ability of the Driftsonde 383
to observe specific phenomena depends critically upon finding a suitable launch site relative to 384
stratospheric wind patterns. For T-PARC, finding a subtropical Pacific island for which 385
stratospheric wind patterns intersected the climatological tracks of tropical cyclones was 386
surprisingly difficult. In contrast, finding a suitable launch site for AMMA within Africa was more 387
straightforward. Once a launch site is selected, the success of the Driftsonde to target a specific 388
event depends on accurate forecasts of both the wind field in the stratosphere and the 389
evolution and movement of the event to be targeted. Despite the ability of Driftsondes to 390
intercept tropical cyclones during AMMA and to a lesser extent during T-PARC, reliance upon 391
forecasts with lead times of several days is a disadvantage relative to aircraft dropsonde 392
deployment. At far longer lead times, the Driftsonde behavior from CONCORDIASI and 393
experience from ballooning campaigns during GARP suggest that the balloons tend to be 394
22
advected into the confluent, more dynamically active regions of the atmosphere. For many 395
aspects of weather research, this behavior is desirable. 396
Despite these complexities, scientifically, the Driftsondes are well suited to numerous 397
applications, especially because of their ability to operate in otherwise data-sparse regions. In 398
particular, they have unique value for verifying and evaluating NWP models, global reanalysis 399
models, and data assimilation approaches. The measurements are also a valuable resource to 400
validate remote sensors, especially on satellites but also airborne or ground based remote 401
sensors. Driftsondes also can support process studies in otherwise difficult locations. In AMMA 402
and T-PARC, examples are effects of the SAL and factors that control the development of a 403
tropical disturbance. There is also a potential role for Driftsonde operationally, although costs 404
and forecast impacts of this have not been considered in detail. For example, a concept 405
discussed in the early years of Driftsonde was that a series of Driftsondes could be released at 406
regular intervals from sites in Asia to provide synoptic data over the Pacific Ocean, or from the 407
east coast of the United States for regular observations over the Atlantic Ocean. In addition to 408
Driftsonde flights, the Concordiasi program included measurements of ozone-related processes, 409
microphysics of stratospheric clouds, and remote sensing using GPS occultation. It showed the 410
potential of combining such diverse flight level measurements with the vertical profiles from 411
dropsondes to carry out a multi-disciplinary experiment that would not be possible with 412
aircraft. 413
The Driftsonde System has been discussed as a possible contributor to future field 414
studies. One is a long-duration stratospheric balloon campaign at the equator intended to 415
23
study, among other goals, the dynamics of the equatorial middle atmosphere with a focus on 416
the quasi-biennial oscillation, and transport, dehydration, and clouds in the tropical tropopause 417
layer. A second field study suggested Driftsondes as one of a synergistic set of tools to study the 418
propagation and effects of orographically generated atmospheric gravity waves from near the 419
surface to the upper atmosphere. Those with interest in using Driftsondes in their research are 420
encouraged to contact the lead authors. 421
24
Acknowledgements 422
Development and field use of the Driftsonde System is a joint effort of many people, 423
institutions, and nations. We thank all who made the development and deployments to AMMA, 424
T-PARC, and Concordiasi successful. We are grateful to Rolf Langland, Mark Bradford, Joe 425
VanAndel, Dean Lauritsen, Chip Owens, Clayton Arendt, and Mary Hanson for contributions to 426
the development. 427
Melvyn Shapiro is especially acknowledged for his resurrection of the early ideas of the 428
late Vin Lally, which were developed decades before their time. In many regards, this paper is a 429
testament to Vin’s creativity. 430
We are grateful for funding support from the National Science Foundation’s Division of 431
Atmospheric and Geospace Sciences and Office of Polar Programs (Grants ATM-0301213, ATM-432
9732665, ANT-0733007, ANT-1002057, and AGS-0736003); National Oceanographic and 433
Atmospheric Administration (Grant NA17GP1376); National Science Council of Taiwan (Grants 434
NSC 96-2745-M-002-004, NSC 97-2111-M-002-005, and NSC 97-2111-M-002-016-MY3); Taiwan 435
Central Weather Bureau (Grant MOTC-CWB-97-6M-01); Office of Naval Research (Grant 436
N00173-08-1-G007 and N00014-09-WR20008), and the support of the national and 437
international THORPEX Project Offices. NSF further supported these field projects through their 438
support of the US THORPEX Project Office, and the Lower Atmospheric Observing Facilities. 439
The National Center for Atmospheric Research is sponsored by the National Science 440
Foundation. 441
25
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30
Tables 526
Table 1: MIST dropsonde characteristics 527
MIST sonde Weight: 175 g
Length: 30.5 cm
Diameter: 4.6 cm
Pressure, temperature, and dual-
humidity sensors (used for T-PARC
and Concordiasi, not AMMA)
Vaisala module RSS921 (same as in RS92 radiosonde)
Sample rate: 0.5 s
Resolution: P: 0.01 hPa, T: 0.01o, H: 0.1%
Wind speed and direction GPS
Sample rate: 0.25 s
Resolution: 0.01 ms-1 and 0.1o
Sonde fall speed Approx. 90 ms-1 at 30 km, 45 ms-1 at 20 km, and 10 ms-1
at sea level
Sonde fall time Approx. 19 minutes from 30 km, 16 minutes from 20 km
528
31
Table 2: Driftsonde evolution through three field projects 529
African Monsoon Multidisciplinary Analyses (AMMA) August-September, 2006
Launch site: Zinder, Niger
Superpressure balloon. 8 flights. 3-18 day duration. 20 km float level.
178 MIST sondes with T, RH, GPS winds. No pressure sensor
Ground control through a terminal modem program with simple text commands and
manual operation.
THORPEX-Pacific Asian Regional Campaign (T-PARC) August-October, 2008
Launch site: Hawaii (the big Island)
Zero pressure balloon. 15 flights. 3-6 day duration. 30 km float level.
254 MIST sondes with P, T, RH, GPS winds (equivalent to Dropsonde sensor suite)
Web-based ground control for drops and display position and sounding data
Concordiasi Field Experiment, September-December, 2010
Launch site: McMurdo Station, Antarctica
Superpressure balloon. 13 flights. 50+ day duration. 18 km float level.
644 MIST sondes with P, T, RH, GPS winds (equivalent to Dropsonde sensor suite)
Enhanced web-based ground control to schedule automatic drops and display position and
sounding data
530
32
Figure Captions 531
Figure 1: The Driftsonde System concept 532
Figure 2: AMMA Driftsonde flight train 533
Figure 3: Driftsonde gondola 534
Figure 4: Sample Driftsonde temperature profiles, with the drop altitudes of Driftsonde and the 535
T-PARC aircraft 536
Figure 5: Four images of Driftsonde deployments. (a) Launch from McMurdo Station, Antarctica 537
during Concordiasi (2010); (b) Shortly after launch during Concordiasi. Dropsondes are visible at 538
perimeter of the Driftsonde gondola below the CNES superpressure balloon; (c) Launch from 539
Hawaii during T-PARC (2008). The Driftsonde gondola is on its deployment sled; (d) Driftsonde 540
before launch during AMMA (2006). This earlier version of the Driftsonde gondola was 541
constructed from cardboard rather than hard foam. 542
Figure 6: Trajectories of the 8 Driftsondes launched from Zinder, Niger, located 640 km east of 543
Niamey. Squares indicate the location of a dropsonde release. 544
Figure 7: Vertical profiles of relative humidity (a), temperature difference (b), zonal wind (c) and 545
meridional wind (d) from the ARPEGE (ARP) and ECMWF Integrated Forecast System (IFS) 546
model analyses co-located with dropsondes (DROP) within the Saharan Air Layer. 547
Figure 8: Locations of dropsondes deployed from the 16 Driftsonde balloons launched from the 548
Big Island of Hawaii during T-PARC. Squares indicate the location of a dropsonde release. 549
33
Figure 9: Infrared satellite image of a tropical disturbance at 0500 UTC 29 August 2008 over 550
which the Driftsonde (yellow drift track, progressing east to west) was deploying dropsondes 551
(yellow balloon symbols). The Air Force C-130 (black flight track) also released dropsondes for 552
this event (black/white squares). Driftsonde releases occurred between 00 and 09 UTC, while 553
Aircraft releases were between 00 and 05 UTC. The NRL P-3 aircraft (not shown) also collected 554
data in the environment surrounding this disturbance. 555
Fig. 10: Locations of all 644 dropsondes (yellow squares) released over Antarctica during 556
Concordiasi and radiosonde stations (red circles) on the Antarctic continent (top); Flight tracks 557
of the 13 Driftsondes for the duration of the project (middle); and tracks of the Driftsondes 558
constellation during a single 12 hour period on November 26, 2010 showing the wide 559
distribution of possible release points (bottom). 560
Fig. 11 Mean (solid line) and standard deviation (dashed line) of temperature differences 561
between satellite and dropsonde (red line) or radiosonde (black line) data for NOAA IASI 562
instrument (left panel) and AIRS (right panel) products. 563
Figure 12: The difference between the dropsonde and the model temperatures at the lowest 564
model level for the French global model. Blue colors indicate that the dropsonde is colder than 565
the model, and red colors indicate that it is warmer. 566
Figure 13: The total impact of dropsonde temperature (T) and wind is illustrated at high levels 567
(pressure less than 400 hPa) and low levels (pressure less 400 hPa) in the left panel, together 568
with the number of observations in the right panel. Negative values of the impact indicate that 569
the data contribute to reducing the error in the NWP system. For observations, each individual 570
34
datum on each pressure level is counted; for winds, zonal and meridional components are 571
counted separately. The impact has been measured using adjoint-based sensitivity of the 24-572
hour forecast error with respect to observations. The forecast error has been defined using a 573
dry total energy norm over the polar area (south of 60oS) and from the surface to the top of the 574
model. The linear estimation has been computed using a second-order approximation. 575
35
Figures 576
577
Figure 1: The Driftsonde System concept 578
36
579
Figure 2: AMMA Driftsonde flight train 580
37
581
Figure 3: Driftsonde gondola 582
System Electronics
Lithium Batteries
Battery & Elect. Heater
Iridium Modem
MIST Sondes
GPS & Iridium Antenna
400 MHz Sonde Antenna
Solar Panels for Heater
NOT TO SCALE
Harness
38
583
Figure 4: Sample Driftsonde temperature profiles, with the drop altitudes of Driftsonde and the 584
T-PARC aircraft 585
39
586
Figure 5: Four images of Driftsonde deployments. (a) Launch from McMurdo Station, Antarctica 587
during Concordiasi (2010); (b) Shortly after launch during Concordiasi. Dropsondes are visible at 588
perimeter of the Driftsonde gondola below the CNES superpressure balloon; (c) Launch from 589
Hawaii during T-PARC (2008). The Driftsonde gondola is on its deployment sled; (d) Driftsonde 590
before launch during AMMA (2006). This earlier version of the Driftsonde gondola was 591
constructed from cardboard rather than hard foam. 592
d
a
c
b
40
593
Figure 6: Trajectories of the 8 Driftsondes launched from Zinder, Niger, located 640 km east of 594
Niamey. Squares indicate the location of a dropsonde release. 595
41
596
Figure 7: Vertical profiles of relative humidity (a), temperature difference (b), zonal wind (c) and 597
meridional wind (d) from the ARPEGE (ARP) and ECMWF Integrated Forecast System (IFS) 598
model analyses co-located with dropsondes (DROP) within the Saharan Air Layer. 599
Meridonal wind (m s-1)
Zonal wind (m s-1)
Temperature difference (K)
Relative Humidity (%)
42
600
Figure 8: Locations of dropsondes deployed from the 16 Driftsonde balloons launched from the 601
Big Island of Hawaii during T-PARC. Squares indicate the location of a dropsonde release. 602
43
603
Figure 9: Infrared satellite image of a tropical disturbance at 0500 UTC 29 August 2008 over 604
which the Driftsonde (yellow drift track, progressing east to west) was deploying dropsondes 605
(yellow balloon symbols). The Air Force C-130 (black flight track) also released dropsondes for 606
this event (black/white squares). Driftsonde releases occurred between 00 and 09 UTC, while 607
Aircraft releases were between 00 and 05 UTC. The NRL P-3 aircraft (not shown) also collected 608
data in the environment surrounding this disturbance. 609
44
610
611
612
Fig. 10: Locations of all 644 dropsondes (yellow squares) released over Antarctica during 613
Concordiasi and radiosonde stations (red circles) on the Antarctic continent (top); Flight tracks 614
of the 13 Driftsondes for the duration of the project (middle); and tracks of the Driftsondes 615
45
constellation during a single 12 hour period on November 26, 2010 showing the wide 616
distribution of possible release points (bottom). 617
46
618
Fig. 11 Mean (solid line) and standard deviation (dashed line) of temperature differences 619
between satellite and dropsonde (red line) or radiosonde (black line) data for NOAA IASI 620
instrument (left panel) and AIRS (right panel) products. 621
47
622
Figure 12: The difference between the dropsonde and the model temperatures at the lowest 623
model level for the French global model. Blue colors indicate that the dropsonde is colder than 624
the model, and red colors indicate that it is warmer. 625
48
626
Figure 13: The total impact of dropsonde temperature (T) and wind is illustrated at high levels 627
(pressure less than 400 hPa) and low levels (pressure less 400 hPa) in the left panel, together 628
with the number of observations in the right panel. Negative values of the impact indicate that 629
the data contribute to reducing the error in the NWP system. For observations, each individual 630
datum on each pressure level is counted; for winds, zonal and meridional components are 631
counted separately. The impact has been measured using adjoint-based sensitivity of the 24-632
hour forecast error with respect to observations. The forecast error has been defined using a 633
dry total energy norm over the polar area (south of 60oS) and from the surface to the top of the 634
model. The linear estimation has been computed using a second-order approximation. 635