Flight model of the BICZEPS instrument

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61389005%3A_____%2F22%3A00570380" target="_blank" >RIV/61389005:_____/22:00570380 - isvavai.cz</a>

Alternative codes found

RIV/27378381:_____/22:N0000003 RIV/68407700:21340/22:00365449

Result on the web

—

DOI - Digital Object Identifier

—

Result language

angličtina

Original language name

Flight model of the BICZEPS instrument

Original language description

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.nThe 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).n

Czech name

—

Czech description

—

Type

G_funk - Functional sample

CEP classification

—

OECD FORD branch

10308 - Astronomy (including astrophysics,space science)

Project

<a href="/en/project/TJ04000374" target="_blank" >TJ04000374: Advanced dosimetry for biological systems in near-earth space</a><br>

Continuities

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year

2022

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Internal product ID

TJ04000374-V2-Gfunk

Numerical identification

TJ04000374-V2

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.

Economical 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%.

Application category by cost

—

Owner IČO

61389005

Owner name

Ústav jaderné fyziky

Owner country

CZ - CZECH REPUBLIC

Usage type

A - K využití výsledku jiným subjektem je vždy nutné nabytí licence

Licence fee requirement

A - Poskytovatel licence na výsledek požaduje licenční poplatek

Web page

—