The AMS-02 Time of Flight System. Final Design
| dc.creator | Bindi, V. | |
| dc.creator | Carota, N. | |
| dc.creator | Casadei, D. | |
| dc.creator | Castellini, G. | |
| dc.creator | Cindolo, F. | |
| dc.creator | Contin, A. | |
| dc.creator | Giovacchini, F. | |
| dc.creator | Giusti, P. | |
| dc.creator | Laurenti, G. | |
| dc.creator | Levi, G. | |
| dc.creator | Martelli, R. | |
| dc.creator | Palmonari, F. | |
| dc.creator | Quadrani, L. | |
| dc.creator | Salvadore, M. | |
| dc.creator | Sbarra, C. | |
| dc.creator | Zichichi, A. | |
| dc.date | 2003-05-26 | |
| dc.date.accessioned | 2026-07-07T03:35:50Z | |
| dc.date.available | 2026-07-07T03:35:50Z | |
| dc.description | The AMS-02 detector is a superconducting magnetic spectrometer that will operate on the International Space Station. The time of flight (TOF) system of AMS-02 is composed by four scintillator planes with 8, 8, 10, 8 counters each, read at both ends by a total of 144 phototubes. This paper describes the new design, the expected performances, and shows preliminary results of the ion beam test carried on at CERN on October 2002. | |
| dc.description | 4 pages, 6 EPS figures. Proc. of the 28th ICRC (2003) | |
| dc.identifier | https://arxiv.org/abs/hep-ex/0305074 | |
| dc.identifier | http://arxiv.org/abs/hep-ex/0305074 | |
| dc.identifier.uri | http://salesiana.dossiersoluciones.com/handle/123456789/37512 | |
| dc.subject | High Energy Physics - Experiment | |
| dc.title | The AMS-02 Time of Flight System. Final Design | |
| dc.type | text |