Purpose of the flight and payload description

SAOZ stands for Systeme d'Analyse par Observation Zenithale and is a UV-visible spectrometer able to provide vertical profiles of O3, NO2, OClO, BrO and H2O by solar occultation during ascent of the balloon (or descent) and from float at 30 km during sunset (or sunrise). The balloon version of the SAOZ instrument is very similar to the one used for ground-based measurements of total ozone and NO2.

It is composed by a commercial flat field, 360mm, holographic grating spectrometer equipped with a 1024-diode linear array and an entrance slit of 50 µm. A simple conical mirror replaces the gondola orientation or sun tracker systems generally used on large balloon platforms and is driven by an on-board computer, connected to a PTU (Pressure, Temperature and Humidity) sensor, a GPS (Global Positioning system ) for the localisation (Altitude, latitude and longitude) and an Argos transmitter for the recovery of the payload after cut-down and descent under parachute.

At left can be seen a picture of the standard package.The weight of the instrument is 20 Kg and is contained in a insulated box with only a small aperture in the top for capture the solar rays. It's currently flown in three configurations, SaOZ-Standard, SAOZ-BrO and SAOZ-H2O each tuned to a different wavelength for measurements of different atmospheric constituents.

The second payload on the balloon was an instrument called DIRAC which stands for Determination In situ by Rapid Analytical Chromatography. It's a portable, lightweight gas chromatograph aimed to perform fast analysis of a single tracer to maximize the vertical resolution of ascent/descent profiles. It was developed by the University of Cambridge based on the techniques used in another instrument called DESCARTES. The sample in DIRAC is collected on a Carboxen trap by passing through it a known volume of air. The use of the carbon based Carboxen adsorbent enables a wide range of halocarbons to be pre-concentrated prior to analysis, thus extending the potential range of measured species. DIRAC has a maximum autonomy of 10 hours and works automatically using a PC-104 embedded computer. Data is stored on board and can also be transmitted to ground via a telemetry link. It's overall weight is 21 kg.

A third instrument onboard was µLIDAR also known as MULID which is the first lightweight balloon-borne microlidar ever built. It was developed by CNR-ENEA to measure the depolarized signal backscattered by cloud particles. It's light source is a solid state laser of 1.5 µJoules of power that operates at a repetition rate of 1 kHz and at a wavelength of 532 nm. The receiver is composed by a Newtonian modified reflector telescope and the detectors are two photo-multipliers modules used to collect the backscattered light and to divide it according to its wavelength. The whole system (weighting 4 kg) is enclosed in an insulating polyurethane shield to reduce heat exchange with external environment and externally covered by a reflecting Mylar microfilm. The gondola final weight including batteries and balloon control systems is of 10 kg.

Details of the balloon flight

Balloon launched on: 5/14/2002 at 17:45
Launch site: Centre de Lancement de Ballons CLBA, Aire Sur L'Adour, Landes, France  
Balloon launched by: Centre National d'Etudes Spatiales (CNES)
Balloon manufacturer/size/composition: Zero Pressure Balloon model 10zl Zodiac - 10.000 m3
Balloon serial number: 10ZL Nº 93
End of flight (L for landing time, W for last contact, otherwise termination time): 5/14/2002 at ~ 21:00
Balloon flight duration (F: time at float only, otherwise total flight time in d:days / h:hours or m:minutes - ): 3 h 13 m
Payload weight: 124 kgs
Gondola weight: 71 kgs

External references

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