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Reactor Core Design & Physics

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International

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This subcontract for the Canadian Space Agency involves the design of nuclear reactor cores and the management of fission physics for lunar microreactor projects. The selected provider will be responsible for performing reactor physics calculations, designing core architecture, and developing essential reactivity control and shutdown mechanisms. A primary focus of the work is ensuring criticality safety and accurate life prediction specifically tailored for lunar environments. The scope of work culminates in the delivery of detailed core design specifications and comprehensive safety analysis reports. This project is categorized under NAICS code 541715 and is to be performed within Canada. Interested parties must adhere to the response deadline of November 23, 2026.

General Info

Canadian Space Agency subcontract for lunar microreactor core design and fission physics management.

Documents

This scope was carved out of 9F055- 20260146.

The full solicitation package (2 documents), including the RFP, is on the prime solicitation, not on this scope.

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Systèmes De Microréacteur Lunaire Canadien

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AgencyGovernment of Canada → Canadian Space Agency
ContactsNo contacts available
OfficeN/A
Office AddressN/A
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Full Description

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Designs nuclear reactor cores and manages fission physics for prime contractors on Canadian Space Agency lunar microreactor projects. Performs reactor physics calculations, designs core architecture, and develops reactivity control and shutdown mechanisms. Ensures criticality safety and life prediction for lunar environments. Delivers core design specifications and safety analysis reports.

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International
Systèmes De Microréacteur Lunaire Canadien
Solicitation # 9F055- 20260146
The Canadian Space Agency (CSA) has issued a Request for Information (RFI) under solicitation number 9F055-20260146 to identify Canadian technologies and capabilities relevant to lunar microreactors and enabling technologies. This initiative seeks to gather evidence-based data on Canada's existing strengths, technology maturity, supply chains, and development pathways to inform future space exploration programs and procurement strategies. The CSA is interested in a wide range of contributions, from complete systems and subsystems to specialized research and consortium roles, and is not requiring a single entity to deliver an end-to-end system. Notional performance parameters of interest include a net continuous electric power of approximately 20-80 kWe and an operational life of 10 years or more. This RFI is not a bid solicitation and will not result in the award of a contract, grant, or funding agreement. Responses are not scored for supplier selection but are used to map the domestic landscape. Interested parties from industry, academia, and research institutions must submit their responses by November 23, 2026. Submissions should follow the recommended format in Annex A and utilize the Capability Matrix and Technology Readiness Level references provided in the attachments. All responses must be unclassified, and any proprietary information must be clearly marked. The CSA emphasizes that future activities must prioritize safety, security, environmental protection, and non-proliferation in accordance with the Nuclear Safety and Control Act and other applicable laws.

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NAICS: 927110
International
Enabling Technology for Future Missions
Solicitation # 9F063-20260085
The Canadian Space Agency (CSA) is soliciting proposals under solicitation number 9F063-20260085 for the development of one to three enabling technologies to support future space missions. The primary objective is to advance strategic technologies to reduce technical uncertainties and support the implementation of future Canadian space activities. A specific focus of this effort is the maturation of a lightweight, athermal reflecting telescope capability to Technology Readiness Level (TRL) 5. This includes the delivery of a reflecting telescope brassboard validated for Low Earth Orbit (LEO) vibration and thermal-vacuum environments, intended for Earth Observation imaging payloads on CubeSats of 4U or larger, with the telescope itself being 2U or less. Key performance targets include a Ground Sampling Distance of less than 7 metres and a swath width greater than 5 km. The project is planned for a duration of 16 months, structured around five key milestones: a Kick-off meeting, Preliminary Design Review, Detailed Design Review/Work Authorization Meeting, Test Readiness Review, and a Final Review meeting. Deliverables include the hardware brassboard, CAD and performance analysis models, software, and a Technology Roadmap for advancing to TRL 6-8. This solicitation is restricted to Canadian suppliers. Awards will be based on the highest combined rating of technical merit (60 percent) and price (40 percent), with a minimum technical score of 70 points required for consideration. The procurement process includes strict requirements for security clearances, intellectual property disclosure, and adherence to environmentally preferable packaging standards.
Space Research and Technology

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