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GERMAN CENTER FOR AEROSPACE E.V. (DLR) has floated a tender for Qyro Peter Satellite Mission Management. The project location is Germany and the tender is closing on 07 Oct 2025. The tender notice number is E21272916, while the TOT Ref Number is 125883887. Bidders can have further information about the Tender and can request the complete Tender document by Registering on the site.
Procurement Summary
Country: Germany
Summary: Qyro Peter Satellite Mission Management
Deadline: 07 Oct 2025
Other Information
Notice Type: Tender
TOT Ref.No.: 125883887
Document Ref. No.: E21272916
Financier: Self Financed
Purchaser Ownership: Public
Tender Value: Refer Document
Purchaser's Detail
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Login to see detailsTender Details
The qyro Project is a joint effect of Robert Bosch GmbH, Q.ant, Trumpf Photonic Components, Trumpf Laser Berlin, Ferdinand-Braun-Institut, Leibniz Institute for High Frequency Technology (FBH), and the German Aerospace Center Galileo Competence Center (DLR-GK). Its purepose is to promote germany's role in the space sector by demonstrating the performance of a miniaturised next generation quantum optical gyroscope and therefore pave the way for a commercial use of this new technology for a German company on the promising New Space market. Therefore, the project shall design and develop a miniaturized, high precision nuclear magnetic resonance (NMR) Gyroscope for the use in the satellites. This quantum-based gyro QYRO shall be launched and validated in space against state-of-the-art attitude determination systems for CubeSat missions. For that purpose, DLR's task in this project is to establish the definition and design of the mission to host the QYRO unit. Followed by supporting the other project partners to manufacture a space qualified version of the ground based QYRO unit. Additionally, DLR-KN with the support from GK, will integrate GALANT phased array antenna for space positioning applications, which additionally will be investigated in a first approximation to make the interference detection function usable in space. The payload will be constituted by two QYRO units, the GALANT electronics module together with its antenna module, a reference gyroscope and finally a payload computer. The mission will be launched into an SSO with an apoapsis and periapsis height between 400 and 550 km. In terms of operations, communications and the payload on-board computer software, the valuable experience of DLR-SC and DLR-RB will contribute to a successful operation of the CubeSat. The last stage of the project would comprise launching and operating the CubeSat in space to conduct the in-orbit validation test campaign. The Contractor shall be responsible of providing the M...
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