Purpose of the flight and payload description
Is a Frost Point Hygrometer developed by the Laboratoire de Meteorologie Dynamique (LMD) of France in the late 80's for make "in situ" measurements of the contents of water vapor in the stratosphere. The weak water vapor contents, and the surrounding atmospheric conditions make this kind of measure very difficult and also its necessary to take many precautions to avoid pollution from the balloon and from the payload.
ELHYSA works by the so called chilled mirror technique, in wich the air enters the instrument and circulates over a cooled mirror. The occurrence of dew or white frost is detected in an optical way and the temperature of the mirror is maintained at the temperature of condensation by a feedback loop controlling the cooling and the heating of the mirror using a thermoelectric Peltier device. This temperature, the dew or frost point temperature is directly connected to the partial pressure of water vapor that characterizes the water vapor content of the atmosphere. The simultaneous measurement of the air pressure and air temperature allows the determination of the mixing ratio and the relative humidity.
The use of the Peltier module, provides an autonomous instrument which can be used on long duration balloon flights. However the cooling efficiency of it is strongly dependent on the temperature of the heat sink which is connected to the "hot side" of the module. So, for the long duration flights, CNES developed, a special heat sink composed of a flat metal plate looking upward to the sky, as can be seen in the left image (click to enlarge) so that the instrument is cooled quickly when the sun lays down.
This version of ELHYSA was used in short duration balloon flights until 1993 and in long duration flights -under MIR balloons- until 1996. In later versions the Peltier device was replaced by a system of cooling using liquid nitrogen.
Details of the balloon flight
Balloon launched on: 1/10/1990 at 6:23 utc
Launch site: European Space Range, Kiruna, Sweden
Balloon launched by: Centre National d'Etudes Spatiales (CNES)
Balloon manufacturer/size/composition: Zero Pressure Balloon 12.000 m3
End of flight (L for landing time, W for last contact, otherwise termination time): 1/10/1990
Campaign: CHEOPS 3
This was one of the firsts balloon flight of the CHEOPS-3 campaign. It served to test flight of launch and telemetry procedures for the whole campaign. The scientific team that operated the ELHYSA instrument could not choose the launch conditions: there were gusts of wind with ice crystals on the launch site, and because of recovery constraints measurements ceased at the end of the balloon ascent. No useful data was obtained: though the hygrometer was 100 m below the balloon, water vapour measurements were probably contaminated due to snowy launch conditions.