Flight model instrumentu BICZEPS

0570380 - ÚJF 2023 RIV CZ eng L - Prototype, f. module
Sysala, R. - Suchánek, P. - Brož, P. - Šanda, Z. - Ploc, Ondřej - Kákona, Martin - Sommer, Marek - Lužová, Martina - Marčišovský, M. - Jirsa, J. - Kabátová, A. - Kafka, V. - Marčišovská, M. - Vaculčiak, M. … Total 16 authors
Flight model instrumentu BICZEPS.
[Flight model of the BICZEPS instrument.]
Internal code: TJ04000374-V2-Gfunk ; 2022
Technical parameters: The BICZEPS device consists of two main parts – the Sensor part and the Electronics part. The inputs and outputs to the device are only the power supply +28 VDC, two USB communication lines, and four digital and analog lines indicate the states of the device's basic parameters. The Sensor part contains three main active detectors: Scintillator with PH32 chips Radiation Monitor (SPRM), SpacePix2 Radiation Monitor (SXRM) and Space Dosimeter (SDOS). The Sensor part is powered by the power supplies produced by PWS PCB and communicates with the Electronics part through serial communication buses. The Electronics part contains power management, data processing, and data storage. This part is mechanically mounted to the stack using spacers and M3 screws. Each PCB in the Electronics stack is electrically connected with the connector (52-pin, 2.54 pitch, THT). The flight model is based on the Engineering qualification model of the BICZEPS instrument (TJ04000374-V1) with minor changes in the design which resulted from the EQM verification.
Economic parameters: Tento funkční vzorek je samostatně funkční autonomní detekční instrument určený pro komplexní charakterizaci radiačního pole na nízkých orbitách Země. Rozdělení práv k výsledku je definováno ve smlouvě o využití výsledků uzavřené mezi FJFI ČVUT, UJF AV ČR a evolving systems consulting s.r.o. Podíly práv Smluvních stran na výsledku TJ04000374-V2 jsou: ESC 33%, FJFI 33%, UJF 33%.
R&D Projects: GA TA ČR(CZ) TJ04000374
Institutional support: RVO:61389005
Keywords : flight model * BICZEPS instrument * space mission * SXRM * SPRM * SDOS
OECD category: Astronomy (including astrophysics,space science)

The Flight Model (FM) is the final version of the BICZEPS instrument which shall perform the measurements during space mission. The Flight Model (or so called flight unit) shall be installed to spacecraft and launched to orbit.
The spacecraft and launch vehicle had to be changed during the project due to change of geopolitical situation. In the time of completion of the final report an alternative mission is being searched. Due to the fact that the instrument was designed for spacecraft with atmospheric condition on board the most suitable spacecraft is the International Space Station (ISS).

Permanent Link: https://hdl.handle.net/11104/0342014