PAMELA is a satellite borne experiment designed to study with great accuracy cosmic rays of galactic, solar, and trapped nature in a wide energy range (protons 80 MeV 700 GeV, electrons 50 MeV 400 GeV). Main objective is the study of the antimatter component: antiprotons (80 MeV 190 GeV), positrons (50 MeV 270 GeV) and search for antimatter with a precision of the order of 10-8. The experiment, housed on board the Russian Resurs-DK1 satellite, was launched on June 15th, 2006 in a 350 × 600 km orbit with an inclination of 70°. The detector is composed of a series of scintillator counters arranged at the extremities of a permanent magnet spectrometer to provide charge, time-of-flight, and rigidity information. Lepton/hadron identification is performed by a silicon tungsten calorimeter and a neutron detector placed at the bottom of the device. An anticounter system is used offline to reject false triggers coming from the satellite. In self-trigger mode the calorimeter, the neutron detector, and a shower tail catcher are capable of an independent measure of the lepton component up to 2 TeV. In this work we describe the experiment, its scientific objectives, and the performance in the first months after launch.
Launch of the Space experiment PAMELA / Barbarino, Giancarlo; Russo, Stefano; DE ROSA, Gianfranca; D., Campana; G., Osteria. - In: ADVANCES IN SPACE RESEARCH. - ISSN 0273-1177. - STAMPA. - 42:(2008), pp. 455-466. [10.1016/j.asr.2007.07.023]
Launch of the Space experiment PAMELA
BARBARINO, GIANCARLO;RUSSO, STEFANO;DE ROSA, GIANFRANCA;
2008
Abstract
PAMELA is a satellite borne experiment designed to study with great accuracy cosmic rays of galactic, solar, and trapped nature in a wide energy range (protons 80 MeV 700 GeV, electrons 50 MeV 400 GeV). Main objective is the study of the antimatter component: antiprotons (80 MeV 190 GeV), positrons (50 MeV 270 GeV) and search for antimatter with a precision of the order of 10-8. The experiment, housed on board the Russian Resurs-DK1 satellite, was launched on June 15th, 2006 in a 350 × 600 km orbit with an inclination of 70°. The detector is composed of a series of scintillator counters arranged at the extremities of a permanent magnet spectrometer to provide charge, time-of-flight, and rigidity information. Lepton/hadron identification is performed by a silicon tungsten calorimeter and a neutron detector placed at the bottom of the device. An anticounter system is used offline to reject false triggers coming from the satellite. In self-trigger mode the calorimeter, the neutron detector, and a shower tail catcher are capable of an independent measure of the lepton component up to 2 TeV. In this work we describe the experiment, its scientific objectives, and the performance in the first months after launch.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.