Engineering qualification model of the BICZEPS instrument
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21340%2F21%3A00356053" target="_blank" >RIV/68407700:21340/21:00356053 - isvavai.cz</a>
Result on the web
—
DOI - Digital Object Identifier
—
Alternative languages
Result language
angličtina
Original language name
Engineering qualification model of the BICZEPS instrument
Original language description
This document describes the Engineering Qualification Model (EQM) of the BICZEPS instrument. The purpose of the Engineering Qualification Model (EQM) is to perform qualification tests in order to determine whether the design meets all given requirements and it is able to withstand the space mission. As a result of qualification testing it will be decided whether the design is mature enough to build a Flight Model (FM) unit. A secondary purpose of EQM is to serve as a platform for calibration of radiation sensors. The built EQM unit was primarily used for testing of radiation sensors in the HIMAC facility (Heavy Ion Medical Accelerator in Chiba).
Czech name
—
Czech description
—
Classification
Type
G<sub>funk</sub> - Functional sample
CEP classification
—
OECD FORD branch
10308 - Astronomy (including astrophysics,space science)
Result continuities
Project
<a href="/en/project/TJ04000374" target="_blank" >TJ04000374: Advanced dosimetry for biological systems in near-earth space</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2021
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Internal product ID
TJ04000374-V1-Gfunk
Numerical identification
TJ04000374-V1
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).
Economical parameters
Funkční vzorek je výstupem projektu TA ČR TJ04000374 "Pokročilá kosmická dozimetrie pro biologické systémy". Tento funkčnı' vzorek je samostatně funkčnı' autonomnı' detekčnı' instrument určen pro kvalifikačnı' testy. Na jeho základě bude v dalšı' iteraci vytvořený letový model ze space-grade komponent určený pro komplexní charakterizaci radiačního pole na nízkých orbitách Země. Předběžný odhad přístupu k výsledku: ESC 33%, FJFI 33%, UJF 33%. Rozdělenı' práv k výsledku bude definováno ve smlouvě o využitı' výsledků uzavřené mezi FJFI ČVUT, UJF AV ČR a evolving systems consulting s.r.o.
Application category by cost
—
Owner IČO
68407700
Owner name
České vysoké učení technické v Praze / Fakulta jaderná a fyzikálně inženýrská
Owner country
CZ - CZECH REPUBLIC
Usage type
V - Výsledek je využíván vlastníkem
Licence fee requirement
A - Poskytovatel licence na výsledek požaduje licenční poplatek
Web page
—