Purpose of the flight and payload description
The TRIP (Telescope Raffreddato per lInfrarosso su Pallone) was a balloon-borne cryogenically cooled infrared telescope designed for measuring the Near Infrared Cosmological Background (NIRB) in the 15 µm range at an altitude of approximately 40 km. It was developed by two Italian research institutions affiliated with the National Research Council (CNR): the Istituto per le Tecnologie e Studio delle Radiazioni Extraterrestri, in Bologna and the Istituto di Ricerca sulle Onde Elettromagnetiche, in Florence.
In the image at left we can see an scheme of the instrument (click to enlarge). The telescope had a 250 mm primary mirror with an F/2 focal ratio and was designed to minimize thermal noise through cryogenic cooling. The optical system was a double Cassegrain configuration, and the focal plane included a 32-element linear array of InSb detectors, cooled and stabilized at around 52 K, which allowed a field of view of 1.4 arcmin per pixel over a total view of 49 arcmin.
The cryogenic system operated using liquid helium delivered through a transfer line from an external dewar. The helium gas flow was controlled using electrovalves and pressure transducers to stabilize the detector temperature with high precision. Most internal surfaces, including baffles and optics supports, were cooled to temperatures below 120 K to reduce their thermal emission. The telescope structure itself was enclosed in a multi-layer vacuum-insulated cryostat, which also housed a rotating shutter to prevent ice formation during ascent and on-ground tests.
A filter wheel positioned in front of the detector carried seven passband filters and one dark filter, enabling differential measurements to separate various background contributions (zodiacal emission, starlight, and atmospheric emission). Observing strategies included zenith, galactic, and ecliptic scans to isolate different components of the background. The system relied on in-flight calibrations using internal lamps and natural celestial sources, with calibration sequences designed to track and raster-scan calibration stars.
The payload, weighing about 850 kg, was suspended within a gondola and stabilized in azimuth using a magnetometer-controlled system. The elevation was independently controlled, and angular resolution was monitored using a CCD aspect camera. Electronics onboard included two CPUs: one for general experiment control and telemetry, and the other for detector control and data acquisition. A 16-bit ADC converted detector output, and telemetry data were transmitted to ground in real time, where they were analyzed using UNIX and Windows-based software.
Details of the balloon flight
Balloon launched on: 7/25/1990 at
Launch site: Base di Lancio Luigi Broglio, Trapani, Sicily, Italy
Balloon launched by: Centre National d'Etudes Spatiales (CNES)
Balloon manufacturer/size/composition: Zero Pressure Balloon Zodiac - 400.000 m3
End of flight (L for landing time, W for last contact, otherwise termination time): 7/26/1990
Balloon flight duration (F: time at float only, otherwise total flight time in d:days / h:hours or m:minutes - ): 20 h 22 m
Landing site: In Spain
Campaign: ODISSEA 90
Payload weight: 1057 kg
Gondola weight: 707 kg
External references
- Large Heavy Duty Balloons in Europe 10th ESA Symposium on European Rocket and Balloon Programmes and Related Research, Pag. 287
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