Evolution in Design of a Smart Balloon
for Lagrangian Air Mass Tracking
Randy Johnson
NOAA, Air Resources Laboratory,
Field Research Division, Idaho Falls, Idaho 83402
email: randy@noaa.inel.gov |
Steven Businger
University of Hawaii, Honolulu, Hawaii 96822
email: businger@soest.hawaii.edu |
ABSTRACT
A series of balloons, designed at NOAA Air Resources Laboratory Field Research
Division, was released from ship-board during three recent atmospheric
chemistry field experiments to provide Lagrangian air-mass tracking information.
The position of the balloons was monitored via an onboard GPS receiver
and transmitted via radio to a research aircraft operating in the vicinity
of the balloons. In total, seven successful Lagrangian experiments have
been carried out, two each during the ASTEX* and ACE-1* field programs
and three during the ACE-2* field program. This poster reviews and contrasts
the design and capability of the Lagrangian balloons and their performance
during the field experiments.


ASTEX-
was held in the Azores Islands to study the evolution of clean air emanating
fron the north Atlantic. The ASTEX tetroon is a simple constant-level balloon
made of Mylar (trademark) with a tetrahedral shape to facilitate construction
(Fig. 1) (Businger et al. 1996). The
advantage of these tetroons is their small size, ease of deployment, and
low cost. Only GPS position data are available in this design. The disadvantage
of the ASTEX tetroon is the lack of ability to compensate for the impact
of precipitation loading and radiation on the buoyancy of the tetroons
(Fig. 2a and Fig
2b).
ACE-1
- The ACE-1 design of Lagrangian marker tetroon includes control of balloon
lift by the action of a pump and release valve on an internal pressurized
ballast bladder (Fig. 3) (Johnson, Carter,
and Businger 1998, Businger et al. 1998). This design, referred to as a
smart tetroon design, allows the tetroon buoyancy to automatically adjust
when the tetroon travels vertically outside a range of pressures set prior
to release. 
The
ACE-1 deployment in the vicinity of Tasmania, Australia, was the first
for the smart tetroon design (Fig. 4a
and Fig 4b). The ACE-1 tetroons provided
GPS location, barometric pressure, air temperature, relative humidity,
and tetroon status data transmitted via a transponder to a receiver aboard
the NCAR C130 research aircraft flying in the vicinity of the tetroons
to study the evolution of clean air. These data provide tetroon location,
meteorological information on the air parcel and data to help understand
the operation of the smart balloons. The ACE-1 tetroon design proved to
have insufficient dynamic lift range to overcome the combined impact of
water loading and radiational cooling at night, causing the tetroons to
descend near the surface until after sunrise (Fig.
4a).

ACE-2
- Significant design improvements were incorporated into the second-generation
smart balloon (Fig. 5), deployed during
ACE-2 field program held between the coast of Portugal and the Canary Islands
to study the evolution of polluted air emanating from Europe (Fig.
6a) (Johnson, Carter, and Businger 1998). These improvements include
(i) a stronger outer shell to significantly increase dynamic lift range,
(ii) two-way communication with the balloon to allow interactive control
of the balloon operating parameters by an observer, and (iii) a spherical
design to reduce exposure to precipitation. In addition to the variables
transmitted by the ACE-1 tetroon, the ACE-2 balloon provides balloon temperature,
balloon superpressure, and solar radiation data.
The
success of the ACE-2 balloon in maintaining altitude despite condensation
loading and radiational effects is noteworthy (Fig.
6b). The stronger balloon shell provides an order of magnitude increase
in dynamic lift range over the ACE-1 design. The altitude control works
during night and day even when the wetness sensor shows condensation on
the surface of the balloon.
CONCLUSIONS
The second-generation smart balloon design provides the means to track
a parcel of air at a chosen altitude by varying the density of the balloons
as environmental conditions demand. The dynamic range afforded by the high
strength spherical shell in the ACE-2 design allows the balloon to remain
within desired altitude operating limits despite the impacts of condensation,
light precipitation, and radiative cooling. A suite of balloon-borne instruments
can provide useful in situ and radiometric meteorological data, and two-way
commun-ication with the balloon allows interactive control of the balloon
operating parameters by an observer. The available in situ data combined
with the balloon's dynamic range enable the balloon transponder to be programmed
to remain at a constant altitude, to follow an isobaric or isentropic surface,
or to perform soundings. These capabilities and the economical cost of
the design make the smart balloon an attractive platform for a range of
applications in atmospheric chemistry and mesoscale meteorology. Future
improvements in the design and deployment strategy are focused on making
the smart balloon a platform for studying storms. For example, to provide
critical protection from the elements, a transponder design change that
allows it to fit inside the balloon is being considered
* The Atlantic Stratocumulus Transition Experiment/Marine Aerosol Gas
Exchange (ASTEX/MAGE) field project, and the first and second Aerosol Characterization
Experiments (ACE-1, ACE-2).
*ACKNOWLEDGMENTS*
We are grateful to Harvey Killian, Shane Beard, Steven Chiswell, Mark
Geldmeier, and John Heyman for assistance in the field. Roger Carter
provided programing support for the transponder design. Nancy Hulbirt,
Annette Baerman, and Karsten Suhre contributed to the graphics. This
research is a contribution to the International Global Atmospheric Chemistry
(IGAC) Core project of the International Geosphere-Biosphere Programme
(IGBP) and is part of the IGAC Aerosol Character-ization Experiments (ACE).
This work is supported by the National Science Foundation under grants
ATM94-19536 and ATM96-10009 and ONR grant N00014-92-J-1285
REFERENCES
-
Businger, S., S.R. Chiswell, W.C. Ulmer, and R. Johnson, 1996: Balloons
as a Lagrangian Measurement Platform for Atmospheric Research, Journal
of Geophysical Research, 101, 4363-4376
-
Johnson, R., R. Carter, and S. Businger, 1998: Evolution of Smart Balloon
Design for Lagrangian Air Mass Tracking, GPS World. In press.
-
Businger, S., R. Johnson, J. Katzfey, S. Siems, and Q. Wang, 1998: Smart
Tetroons for Lagrangian Air Mass Tracking During ACE-1. Journal of Geophysical
Research. In review.
Web layout: Ray Tanabe
2 May 1998
Updated by Derek Funayama
19 August 2002
For more information, contact:
Dr. Steven Businger
University of Hawaii, Dept. of Meteorology
2525 Correa Road, HIG Room #350
Honolulu, HI 96822
Email: businger@soest.hawaii.edu