Project detail
Polohovací mechanismus pro optickou komunikaci mezi satelity (CPA)
Duration: 1.1.2020 — 30.6.2022
Funding resources
Technologická agentura ČR - Program průmyslového výzkumu a experimentálního vývoje TREND
- whole funder (4. 3. 2020 - 30. 6. 2022)
On the project
The Coarse Pointing Assembly (CPA) is a two axis beam deflecting system which when integrated with the telescope provides a periscope form of coarse pointing. The CPA will provide the large angular view ranges of the Field of Regard (FOR) and provide the low bandwidth means of control of the OISL Terminal line of sight.
Description in English
The aim of the project is to develop, manufacture and test a functional sample of a Coarse Pointing Assembly for optical inter-satellite communication. The mechanism is meant to be a part of new product line aiming at satellite constellations. The important requirement of the design activities is the acceptable price which is expected to be dramatically lower than for traditional space mechanisms.
That requirement is dictating a use of parts, components, manufacturing processes that are not traditionally used in space. The technical risk related to use of non-space items is to be minimized by involving detailed analyses supported by vast test campaign.
Keywords
Coarse pointing assembly, CPA, APM, aerospace, space,
Key words in English
Pointing assembly, inter-satellite laser communication, precision manufacturing, space, bearings, process optimization
Mark
FW01010297
Default language
Czech
People responsible
Křupka Ivan, prof. Ing., Ph.D. - principal person responsible
Košťál David, Ing., Ph.D. - fellow researcher
Kvarda Daniel, Ing., Ph.D. - fellow researcher
Šperka Petr, Ing., Ph.D. - fellow researcher
Units
Institute of Machine and Industrial Design
- responsible department (2.7.2019 - not assigned)
Institute of Machine and Industrial Design
- beneficiary (2.7.2019 - not assigned)
Results
KOŠŤÁL, D.; SVOBODA, T.; KŘUPKA, I.: Testování tuhosti ložisek; Testovací stanice pro měření tuhosti ložisek pro vesmírné aplikace. VUT FSI A2/422. (funkční vzorek)
Detail
Responsibility: Křupka Ivan, prof. Ing., Ph.D.