2007
DOI: 10.3103/s1062873807040181
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The NUCLEON experiment: The current status

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Cited by 11 publications
(7 citation statements)
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“…2) are four planes of the charge measurement system, a carbon target, six planes of the energy measurement system using the KLEM method (KLEM system tracker), three double-layer planes of the scintillator trigger system, and a small aperture ionization calorimeter (25 × 25 cm 2 ). Details of the detector design are provided in the articles [33,34,35,36,37]. On December 28, 2014, the NUCLEON detector was launched into a sun-synchronous orbit.…”
mentioning
confidence: 99%
“…2) are four planes of the charge measurement system, a carbon target, six planes of the energy measurement system using the KLEM method (KLEM system tracker), three double-layer planes of the scintillator trigger system, and a small aperture ionization calorimeter (25 × 25 cm 2 ). Details of the detector design are provided in the articles [33,34,35,36,37]. On December 28, 2014, the NUCLEON detector was launched into a sun-synchronous orbit.…”
mentioning
confidence: 99%
“…The NUCLEON device [11][12][13][14][15][16] was designed and produced by the collaboration of SINP MSU (the main investigator), JINR (Dubna) and a number of other Russian scientific and industrial centres. Currently, it is placed on board the RESURS-P №2 satellite.…”
Section: The Nucleon Designmentioning
confidence: 99%
“…The "knee" energy range -10 14 -10 16 eV -is a crucial region for the understanding of cosmic rays, acceleration and propagation in the interstellar medium. It is important to obtain more data with elemental resolution.…”
Section: Introductionmentioning
confidence: 99%
“…Two years of the NUCLEON experiment A. Panov tem, and a small aperture calorimeter (IC). Details of the detector design are provided in the articles [34,35,36,37,38]. The weight of the detector is approximately 360 kg; the power consumption does not exceed 160 W. On December 28, 2014, the NUCLEON detector was launched into a sun-synchronous orbit with an average altitude of 475 km and an inclination of 97 degrees as an additional payload of the Russian satellite Resource-P 2.…”
Section: Pos(icrc2017)1094mentioning
confidence: 99%