For BOOMERANG (Balloon Observations of Millimetric Extragalactic Radiation and Geophysics)

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Launch site:Williams Field, McMurdo Base, Antarctica  
Launch team: National Scientific Balloon Facility (NSBF)
Balloon: Long Duration Balloon
Volume: 1.000.000 m3
Serial number: -
Flight identification number: -
Campaign: - 
Payload weight: 3650 lbs
Gondola weight: -
Overall weight: 4739 lbs

The balloon was launched from Williams Field, by dynamic method assisted by launch vehicle on December 29, 1998.

After a nominal ascent phase the balloon achieved the float altitude of 120.000 feet and for the next 10.5 days it floated slowly around the Antarctica in an anti-clockwise flight path at such altitude.

Finally, after a complete circle around the south pole, the flight was terminated and the payload landed 50 km from McMurdo base, for an easy recovery.

The same day the recovery crew traveled in helicopter to the landing site and readied the payload for its trip back to the base.  

BOOMERANG (Balloon Observations of Millimetric Extragalactic Radiation and Geophysics)

Responsable institution:  University of Rome, la Sapienza / California Institute of Technology
Principal Investigator:  Prof. Paolo de Bernardis / Dr. Andrew Lange

This telescope is the culmination of a great cooperative effort between Italian and American teams. It was designed to have the angular resolution and sensitivity necessary to measure the angular power spectrum of anisotropy in the cosmic microwave background at sub-degree scales, a region where there is a wealth of cosmological information.

The telescope consists of a 1.3m off-axis paraboloidal mirror feeding a pair of cold (1.5 K) ellipsoidal mirrors which reimage the prime focus onto an array of feed horns. These concentrate the incoming radiation onto bolometric detectors, cooled to 0.3 Kelvin by a helium refrigerator.

The pointing system consists of a pair of flywheels which torque the telescope against the flight train of the balloon. The rotation rate is adjusted via feedback from rate gyroscopes, a magnetometer, and tilt sensors. The telescope is fully pointable in azimuth, and can tip between 35 and 55 degrees in elevation. An on-board optical star-tracking camera allows accurate post-flight reconstruction of pointing.