Developed by Centre National d'Etudes Spatiales (CNES) / Laboratoire de Météorologie Dynamique (LMD) / Laboratoire de Physique et Chimie de l'Environnement et de l'Espace (LPCE-CNRS)
Balloon launched on 11/27/2019, from Seychelles International Airport, Mahe
Description of the payload
Strateole-2 is a French-US project to study climate processes in the Tropical Tropopause Layer (TTL) and in the lower stratosphere. The project is based in the use of CNES superpressure balloons, capable of drifting for several months between 18 and 20 km altitude. The effort will release a total of nearly 50 long-duration balloons in three separate campaigns between 2019 and 2024. During each Strateole-2 campaign two series of balloons were flown at different altitudes: one above the tropopause -the boundary between the troposphere and the stratosphere- nomenclated as STRAT at about 20,000 metres and the other at around 18,000 metres, at the top of the tropopause nomenclated as TTL. The first series of flights focuses primarily on remote measurements, and the second on in-situ measurements.
Strateole 2 balloons are 11 or 13 metres in diameter and can carry payload gondolas weighing 22 kilograms. Their closed envelope is filled with helium which expands during its ascent, giving it a spheroid shape when it reaches its ""ceiling"" altitude. These superpressure balloons can fly for very long time in the stratosphere, the flight duration being ultimately determined by helium leak or diffusion through the balloon envelope. The target flight duration for Strateole-2 was 3 months.
Each balloon carried a parachute, separator, venting valve, ballast dispenser and two gondolas: EUROS and ZEPHYR
EUROS is a service gondola that hosts and control all devices and systems that ensures the flights are conducted in complete safety for aviation and populated areas overflown and enables the operators to check that the balloon and its systems are functioning correctly. The gondola has its own solar power systems, global communications links (Iridium and Inmarsat), GPS receiver, processing units and a suite of sensors and active control systems including a high-precision air pressure and temperature sensing system. All of these systems have a dual operational and scientific vocation.
The scientific instruments are carried by the ZEPHYR gondola, developed by LMD, LATMOS and DT-INSU. The role of ZEPHYR is to ensure that all scientific instruments are able to perform nominally during the 3-month balloon flights in the stratosphere. Hence, Zephyr provides basicaly a thermal insulation between the instrument electronics and the atmosphere using a 8-cm thick styrofoam box. Also provides renewable power management using solar panels to recharge batteries during day, while the batteries provide sufficient power to handle nighttime activities; positioning and timing thanks to an onboard GPS receiver; communication to the ground control center using an Iridium platform to both download scientific data collected onboard and upload tele-commands from the ground.
Due to payload mass constraints, not all the scientific instruments can be used on all flights. Four combinations of instruments have therefore been devised to achieve the project's science goals.
In this particular flight, the instruments on board were:
SAWfPHY (Surface Wave Acoustic Frost-Point HYgrometer) developed by the Laboratoire de Météorologie Dynamique (LMD). Is a frost-point hygrometer aimed to measure water vapour in the atmosphere in long-duration balloon flights.
BBop (BalloonBorne Ozone Photometer) also developed at LMD. An instrument that detects ozone, which traces the "age" of the air mass, by measuring attenuation of a luminous ultraviolet signal.
LOAC (Light Optical Aerosols Counter) developed by Laboratoire de Physique et Chimie de l'Environnement et de l'Espace (LPCE-CNRS) from France. Is an aerosol counter that measures particles present at the balloon's flight altitude.
TSEN and GPS provided by LMD. Instruments to obtain in-situ values of pressure, temperature and winds.
Video of the launch operations and ascent of the balloon
Details of the balloon flight and scientific outcome
Launch site: Seychelles International Airport, Mahe
Balloon launched by: Centre National d'Etudes Spatiales (CNES) Balloon manufacturer/size/composition: Super Pressure Balloon 11 m diameter Flight identification number: 04-TTL1
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