Canadensys Aerospace Corporation develops space instruments, avionics and mobility systems in Ontario. Its NISA camera family combines compact imaging hardware, onboard storage and image processing for missions with constrained mass, power and communications. The company also supplies spacecraft avionics and onboard computers, develops lunar rovers and instruments, and produces terrestrial RAPTOR unmanned and HAWC optionally crewed vehicles.
The strongest public mission evidence is specific: ILOA credits Canadensys’s ILO-X payload with returning lunar descent and surface images during the 2024 IM-1 mission, while Canadensys reported delivery of a multispectral microscope to Johns Hopkins APL for the separate Lunar Vertex mission. Its ground-vehicle business provides a further route to market: the company reported completing a RAPTOR shipment to a European defence customer in October 2024. Lunar utility vehicles, agriculture modules and tritium heating units have their own development milestones and should be assessed separately from these delivered instruments and vehicles.
Operating context
Mission hardware must be selected by configuration and demonstrated stage. The April 2025 NISA datasheet gives -25 to +50 C operation, 12 MP imaging, 64 GB storage or 32 GB in high-reliability mode, and RS-422, USB 2.0 and Ethernet-over-USB interfaces. Its survival entry says only “extended survival range”; the live webpage retains -200 to +70 C. The PDF’s 50×50×30 mm body-with-lens-holder dimension and the webpage’s 50×50×39 mm with lens use different references. Integration therefore needs an agreed drawing and qualification envelope.
ILO-X returned lunar images in 2024, then stopped when its lander lost power; that flight does not establish lunar-night endurance. APL identifies Canadensys’s Lunar Vertex microscope and a launch no earlier than 2026. ILOA’s current page expects ILO-1 operation beginning in 2029, later than the issuer’s original 2027 plan. Both future mission schedules remain plans.
CSA has ended the first Canadian Lunar Rover Mission. The separate utility rover remains in concept development for the 2030s, with Canadensys performing preparatory and technology-development work. Agriculture activity includes lunar ground-demonstrator design refinement and a Growcer-led Nunavut concept study. The CNL collaboration is for tritium heater development; no delivered heater, quantified heat output or flight qualification was established.
Canadian footprint
Canadensys lists its corporate headquarters at 10 Parr Boulevard in Caledon, Ontario; its camera datasheet and government award use Bolton for that same address. A second facility is at 753 Ontario Street in Stratford, Ontario. The company describes more than 30,000 square feet of office, laboratory, clean-room and integration space supporting design, testing, subsystem qualification and system acceptance work, and identifies Stratford as a RAPTOR production location. The source does not allocate the total floor area between sites or establish current staffing.
Bolton, Ontario is the published city-level context for Canadensys Aerospace. It does not imply a street address or exact facility location.
Canadensys offers two useful routes into the Canadian supply base: compact space instruments with documented lunar-image return, and terrestrial mobility platforms with reported export deliveries and an integrator channel. A buyer or partner can assess the demonstrated instrument and vehicle configuration while separately negotiating development milestones for larger lunar systems. Ontario integration and test facilities support that work, but camera flight use cannot qualify a rover, a heater or an agriculture system. The practical next step is a configuration and acceptance review tied to the funded program, operating environment and support responsibilities.
Interpretation of the public record. Not qualification, endorsement or evidence of buyer interest.
Unmanned and optionally crewed terrestrial mobility platforms
Read technical summary
Canadensys’s terrestrial vehicle family applies lunar mobility design methods to ground operations. RAPTOR is a six-wheeled electric-drive unmanned platform with an open deck for cargo, sensors or other mission payloads; HAWC shares the base platform but adds seating and controls for human driving. The dated RAPTOR brochure lists a 1000 kg payload, 2700 kg gross vehicle weight, 30 km/h speed and optional diesel-generator power. These figures describe that configuration and are not an independently tested autonomous operating envelope.
Canadensys reported completing an order for an unnamed European defence customer in October 2024 and earlier US and European exports. Chironix separately lists RAPTOR as a platform for logistics and security with PilotOS integration. A proposed use still needs confirmation of the current vehicle build, payload and power allocation, autonomy package, terrain limits and buyer acceptance.
Evidence of maturity
Supplier-reported completed European defence-customer shipment in October 2024; independent integrator offering is visible. Buyer acceptance and autonomous field performance were not established.
Commercial availability
RAPTOR and HAWC export supply is reported by Canadensys, and RAPTOR is listed by Chironix. Current configuration, price, production capacity and lead time require quotation.
Canadensys supplies compact NISA cameras and mission instruments and develops lunar mobility systems. NISA’s onboard processing, scripting and storage let an operator capture images and select compressed or full-resolution returns when bandwidth is limited. The April 2025 indicative 186-degree configuration provides 12 MP imaging and a -25 to +50 C operating envelope; its unspecified extended survival range requires mission-specific confirmation despite wider figures on the live webpage.
ILOA independently documents lunar descent and surface-image return from Canadensys’s ILO-X dual-camera payload in 2024. That mission ended with lander power loss and is distinct from the future Lunar Vertex microscope and ILO-1 instrument suite. CSA’s first Canadian Lunar Rover Mission has ended; the separate utility rover remains a 2030s concept supported by preparatory studies, not a delivered flight rover.
Evidence of maturity
ILO-X lunar image return is independently documented. Lunar Vertex hardware delivery is issuer-reported; APL still identifies a future flight. First LRM is ended; utility rover remains concept development.
Commercial availability
NISA stock or custom configurations and engineering are offered. Mission-specific thermal qualification, instrument acceptance and rover delivery milestones require confirmation.
Core features
12 MP NISA imaging; 64 GB flash or 32 GB high-reliability mode in the April 2025 indicative configuration
Public record
Commercial context
NISA is offered in stock and customized configurations; flight-instrument supply and supplier-reported RAPTOR/HAWC exports are documented. Lunar utility-rover studies, ILO-1 instruments, agriculture demonstrators and tritium heating units remain separate contracted or announced development efforts.
Financing and disclosed activity
Public records establish development contracts rather than a complete financial picture. CanadaBuys lists utility-rover contract CW2394557 at C$4,724,895, awarded 25 July 2025 for Phase 0 and technology development through January 2027. Proactive disclosure lists the same identifier at C$5,173,763.49 with an 11 September 2025 date; the reviewed records do not reconcile the difference. These values are not additive or evidence of recognized revenue. Current ownership, private financing and audited financial scale were not established.
Ecosystem relationships
Agriculture concept-study collaborator
The Growcer Inc.
Canadensys announced in September 2026 that it supports Growcer’s CSA study for a deployable controlled-environment agriculture concept for a potential Inuit-led Nunavut initiative. CSA’s award ceiling of C$745,000 is to Growcer; no deployed Canadensys farm is established.
Instrument development customer
International Lunar Observatory Association
ILOA selected Canadensys to design and build ILO-1 instruments after its ILO-X payload returned lunar images in 2024. ILOA’s current support page describes continuing ILO-1 development on Astrolab FLEX with operations expected in 2029; this is a future mission plan.
Thermal-system development collaborator
Canadian Nuclear Laboratories
Canadensys announced in July 2026 that CNL is collaborating on tritium-based radioisotope heating-unit development. The issuer identifies CNL’s tritium handling and testing expertise; flight qualification, heat-output specifications and hardware delivery were not established.
Reviewed connections
Mission area · Reviewed connectionEvidence strength: Needs Review
The publicly described Space mission systems and robotics offering may be relevant to monitoring or remote-operation use cases; this is a derived mapping for reviewer assessment.
Reviewed connections indicate possible relevance based on public evidence. They do not indicate procurement direction, eligibility, endorsement or customer interest.
Questions for a first conversation
01
Which flight configuration, drawing and qualification evidence establish the required survival temperature and integration envelope?
The newer NISA PDF retains -25 to +50 C operation but omits numerical survival limits, while the live webpage still gives -200 to +70 C and a different dimensional reference.
02
Which funded study, instrument acceptance and launch milestones apply to the proposed mission, and which remain contingent on later program decisions?
CSA ended LRM, the utility rover remains in preparatory development, APL lists Lunar Vertex as a future flight, and ILOA currently expects ILO-1 operations in 2029.
03
What current RAPTOR build, autonomy package, payload-power allocation and buyer acceptance evidence can be supplied for the intended terrain and duty cycle?
Canadensys reports RAPTOR exports and Chironix lists an integration offering, but the buyer is unnamed and the public technical brochure is dated 2021.
04
What measured prototype and qualification milestones must the agriculture systems and tritium heaters pass before an operator can commit to deployment?
The Growcer work funds an agriculture concept, lunar agriculture work refines a ground demonstrator, and the CNL heating-unit announcement supplies no flight qualification or heat-output specification.
Original sources 26 linked records
These records support the organization, its owned capabilities and their reviewed connections. A source count is not a count of independent confirmations.
CSA identifies the first Canadian lunar rover project as ended; its mobility knowledge may be reused on other missions, including the separate utility rover.
CSA identifies the first Canadian lunar rover project as ended; its mobility knowledge may be reused on other missions, including the separate utility rover.
On 15 September 2026 Canadensys announced it is supporting Growcer in a CSA study to conceptually design a deployable controlled-environment agriculture unit for potential future integration into an Inuit-led Nunavut food-security initiative.
Public sources cited · Facts and assessments kept separate · Human review
CSA identifies the first Canadian lunar rover project as ended; its mobility knowledge may be reused on other missions, including the separate utility rover.
CSA identifies the first Canadian lunar rover project as ended; its mobility knowledge may be reused on other missions, including the separate utility rover.
CSA identifies the first Canadian lunar rover project as ended; its mobility knowledge may be reused on other missions, including the separate utility rover.
Supports: Rugged space imaging and lunar robotics · maturity
CSA identifies the first Canadian lunar rover project as ended; its mobility knowledge may be reused on other missions, including the separate utility rover.
Supports: Rugged space imaging and lunar robotics · summary
CSA identifies the first Canadian lunar rover project as ended; its mobility knowledge may be reused on other missions, including the separate utility rover.
The official contact page provides an enquiry form for service provision, technology collaboration, partnerships and other enquiries, alongside the two Canadian facility addresses.
The official contact page provides an enquiry form for service provision, technology collaboration, partnerships and other enquiries, alongside the two Canadian facility addresses.
The official contact page provides an enquiry form for service provision, technology collaboration, partnerships and other enquiries, alongside the two Canadian facility addresses.
The October 2024 export release identifies a RAPTOR UGV at Canadensys’s production facility in Stratford, Ontario, and reports completed shipment of an order to Europe.
Canadensys reported on 23 October 2024 that it shipped the final RAPTOR vehicle in an order from an unnamed European defence customer; this is supplier-reported shipment, without buyer acceptance evidence.
Supports: Profile · defence posture
Canadensys reported on 23 October 2024 that it shipped the final RAPTOR vehicle in an order from an unnamed European defence customer; this is supplier-reported shipment, without buyer acceptance evidence.
Canadensys reported on 23 October 2024 that it shipped the final RAPTOR vehicle in an order from an unnamed European defence customer; this is supplier-reported shipment, without buyer acceptance evidence.
Supports: Profile · description
Canadensys says HAWC shares RAPTOR’s base platform but adds seats and an operator station for human driving, and reports earlier HAWC and RAPTOR exports to US and European customers.
Canadensys reported on 23 October 2024 that it shipped the final RAPTOR vehicle in an order from an unnamed European defence customer; this is supplier-reported shipment, without buyer acceptance evidence.
Supports: Profile · profileData.portfolioScope
Canadensys describes RAPTOR as a six-wheeled electric-drive unmanned ground vehicle with 2700 kg gross vehicle weight including a 1000 kg payload, intended for autonomous operation over urban and off-road terrain.
Supports: Profile · description
Canadensys reported on 23 October 2024 that it shipped the final RAPTOR vehicle in an order from an unnamed European defence customer; this is supplier-reported shipment, without buyer acceptance evidence.
Supports: Profile · dual use posture
Canadensys describes RAPTOR as a six-wheeled electric-drive unmanned ground vehicle with 2700 kg gross vehicle weight including a 1000 kg payload, intended for autonomous operation over urban and off-road terrain.
Supports: Profile · commercial status
Canadensys says HAWC shares RAPTOR’s base platform but adds seats and an operator station for human driving, and reports earlier HAWC and RAPTOR exports to US and European customers.
Supports: Profile · executive relevance summary
Source location: executiveRelevanceSummary
Canadensys reported on 23 October 2024 that it shipped the final RAPTOR vehicle in an order from an unnamed European defence customer; this is supplier-reported shipment, without buyer acceptance evidence.
Supports: Profile · commercial status
Canadensys reported on 23 October 2024 that it shipped the final RAPTOR vehicle in an order from an unnamed European defence customer; this is supplier-reported shipment, without buyer acceptance evidence.
Canadensys reported on 23 October 2024 that it shipped the final RAPTOR vehicle in an order from an unnamed European defence customer; this is supplier-reported shipment, without buyer acceptance evidence.
Supports: Profile · description
Canadensys describes RAPTOR as a six-wheeled electric-drive unmanned ground vehicle with 2700 kg gross vehicle weight including a 1000 kg payload, intended for autonomous operation over urban and off-road terrain.
Supports: Profile · defence posture
Canadensys describes RAPTOR as a six-wheeled electric-drive unmanned ground vehicle with 2700 kg gross vehicle weight including a 1000 kg payload, intended for autonomous operation over urban and off-road terrain.
Canadensys reported on 23 October 2024 that it shipped the final RAPTOR vehicle in an order from an unnamed European defence customer; this is supplier-reported shipment, without buyer acceptance evidence.
Supports: Profile · dual use posture
Canadensys says HAWC shares RAPTOR’s base platform but adds seats and an operator station for human driving, and reports earlier HAWC and RAPTOR exports to US and European customers.
Supports: Profile · profileData.portfolioScope
Canadensys says HAWC shares RAPTOR’s base platform but adds seats and an operator station for human driving, and reports earlier HAWC and RAPTOR exports to US and European customers.
Supports: RAPTOR and HAWC ground vehicles · technical tags
Canadensys describes RAPTOR as a six-wheeled electric-drive unmanned ground vehicle with 2700 kg gross vehicle weight including a 1000 kg payload, intended for autonomous operation over urban and off-road terrain.
Supports: RAPTOR and HAWC ground vehicles · technicaldomainslugs
Canadensys describes RAPTOR as a six-wheeled electric-drive unmanned ground vehicle with 2700 kg gross vehicle weight including a 1000 kg payload, intended for autonomous operation over urban and off-road terrain.
Supports: RAPTOR and HAWC ground vehicles · maturity
Canadensys reported on 23 October 2024 that it shipped the final RAPTOR vehicle in an order from an unnamed European defence customer; this is supplier-reported shipment, without buyer acceptance evidence.
Supports: RAPTOR and HAWC ground vehicles · name
Canadensys says HAWC shares RAPTOR’s base platform but adds seats and an operator station for human driving, and reports earlier HAWC and RAPTOR exports to US and European customers.
Supports: RAPTOR and HAWC ground vehicles · capability type
Canadensys says HAWC shares RAPTOR’s base platform but adds seats and an operator station for human driving, and reports earlier HAWC and RAPTOR exports to US and European customers.
Supports: RAPTOR and HAWC ground vehicles · commercial availability
Canadensys reported on 23 October 2024 that it shipped the final RAPTOR vehicle in an order from an unnamed European defence customer; this is supplier-reported shipment, without buyer acceptance evidence.
Supports: RAPTOR and HAWC ground vehicles · technical tags
Canadensys describes RAPTOR as a six-wheeled electric-drive unmanned ground vehicle with 2700 kg gross vehicle weight including a 1000 kg payload, intended for autonomous operation over urban and off-road terrain.
Supports: RAPTOR and HAWC ground vehicles · summary
Canadensys says HAWC shares RAPTOR’s base platform but adds seats and an operator station for human driving, and reports earlier HAWC and RAPTOR exports to US and European customers.
Supports: RAPTOR and HAWC ground vehicles · slug
Canadensys says HAWC shares RAPTOR’s base platform but adds seats and an operator station for human driving, and reports earlier HAWC and RAPTOR exports to US and European customers.
Supports: RAPTOR and HAWC ground vehicles · core features
Canadensys says HAWC shares RAPTOR’s base platform but adds seats and an operator station for human driving, and reports earlier HAWC and RAPTOR exports to US and European customers.
Supports: RAPTOR and HAWC ground vehicles · summary
Canadensys reported on 23 October 2024 that it shipped the final RAPTOR vehicle in an order from an unnamed European defence customer; this is supplier-reported shipment, without buyer acceptance evidence.
Supports: RAPTOR and HAWC ground vehicles · core features
Canadensys describes RAPTOR as a six-wheeled electric-drive unmanned ground vehicle with 2700 kg gross vehicle weight including a 1000 kg payload, intended for autonomous operation over urban and off-road terrain.
Supports: RAPTOR and HAWC ground vehicles · core features
Canadensys describes RAPTOR as a six-wheeled electric-drive unmanned ground vehicle with 2700 kg gross vehicle weight including a 1000 kg payload, intended for autonomous operation over urban and off-road terrain.
Supports: RAPTOR and HAWC ground vehicles · technology readiness level
Canadensys reported on 23 October 2024 that it shipped the final RAPTOR vehicle in an order from an unnamed European defence customer; this is supplier-reported shipment, without buyer acceptance evidence.
Supports: RAPTOR and HAWC ground vehicles · technicaldomainslugs
Canadensys describes RAPTOR as a six-wheeled electric-drive unmanned ground vehicle with 2700 kg gross vehicle weight including a 1000 kg payload, intended for autonomous operation over urban and off-road terrain.
Supports: RAPTOR and HAWC ground vehicles · summary
Canadensys describes RAPTOR as a six-wheeled electric-drive unmanned ground vehicle with 2700 kg gross vehicle weight including a 1000 kg payload, intended for autonomous operation over urban and off-road terrain.
Supports: RAPTOR and HAWC ground vehicles · technical tags
Canadensys says HAWC shares RAPTOR’s base platform but adds seats and an operator station for human driving, and reports earlier HAWC and RAPTOR exports to US and European customers.
NISA’s 2025-04-28 indicative 186-degree configuration has a 4000 by 3000 imager, 64 GB flash or 32 GB high-reliability mode, a 135 g mass and RS-422, USB 2.0 and Ethernet-over-USB interfaces.
Supports: Profile · operating context
The 2025-04-28 NISA datasheet specifies -25 to +50 C operation and an unspecified extended survival range; it requires each application’s technical parameters to be validated.
Supports: Profile · commercial status
The April 2025 NISA datasheet offers stock or customized cameras for customer requirements, with image, lens, thermal-management, housing, software and integration options.
Supports: Profile · canadian footprint
The April 2025 NISA datasheet identifies Canadensys Aerospace Corporation at 10 Parr Boulevard, Bolton, Ontario, Canada L7E 4G9.
Supports: Profile · description
The 2025 NISA datasheet describes onboard image processing and storage, Asp scripting for automated operation, and colour, mono or multispectral and lens customization.
The 2025-04-28 NISA datasheet specifies -25 to +50 C operation and an unspecified extended survival range; it requires each application’s technical parameters to be validated.
Supports: Profile · commercial status
The 2025 NISA datasheet describes onboard image processing and storage, Asp scripting for automated operation, and colour, mono or multispectral and lens customization.
The 2025-04-28 NISA datasheet specifies -25 to +50 C operation and an unspecified extended survival range; it requires each application’s technical parameters to be validated.
The 2025-04-28 NISA datasheet specifies -25 to +50 C operation and an unspecified extended survival range; it requires each application’s technical parameters to be validated.
The 2025-04-28 NISA datasheet specifies -25 to +50 C operation and an unspecified extended survival range; it requires each application’s technical parameters to be validated.
Supports: Rugged space imaging and lunar robotics · commercial availability
The April 2025 NISA datasheet offers stock or customized cameras for customer requirements, with image, lens, thermal-management, housing, software and integration options.
Supports: Rugged space imaging and lunar robotics · core features
The 2025-04-28 NISA datasheet specifies -25 to +50 C operation and an unspecified extended survival range; it requires each application’s technical parameters to be validated.
Supports: Rugged space imaging and lunar robotics · core features
NISA’s 2025-04-28 indicative 186-degree configuration has a 4000 by 3000 imager, 64 GB flash or 32 GB high-reliability mode, a 135 g mass and RS-422, USB 2.0 and Ethernet-over-USB interfaces.
Supports: Rugged space imaging and lunar robotics · technical tags
The 2025 NISA datasheet describes onboard image processing and storage, Asp scripting for automated operation, and colour, mono or multispectral and lens customization.
Supports: Rugged space imaging and lunar robotics · defence applications
The 2025 NISA datasheet describes onboard image processing and storage, Asp scripting for automated operation, and colour, mono or multispectral and lens customization.
Supports: Rugged space imaging and lunar robotics · technical tags
The 2025 NISA datasheet describes onboard image processing and storage, Asp scripting for automated operation, and colour, mono or multispectral and lens customization.
Supports: Rugged space imaging and lunar robotics · commercial availability
The 2025-04-28 NISA datasheet specifies -25 to +50 C operation and an unspecified extended survival range; it requires each application’s technical parameters to be validated.
Supports: Rugged space imaging and lunar robotics · summary
The 2025 NISA datasheet describes onboard image processing and storage, Asp scripting for automated operation, and colour, mono or multispectral and lens customization.
Supports: Rugged space imaging and lunar robotics · technicaldomainslugs
The 2025 NISA datasheet describes onboard image processing and storage, Asp scripting for automated operation, and colour, mono or multispectral and lens customization.
Supports: Rugged space imaging and lunar robotics · technicaldomainslugs
The 2025 NISA datasheet describes onboard image processing and storage, Asp scripting for automated operation, and colour, mono or multispectral and lens customization.
Supports: Rugged space imaging and lunar robotics · summary
The 2025-04-28 NISA datasheet specifies -25 to +50 C operation and an unspecified extended survival range; it requires each application’s technical parameters to be validated.
Supports: Rugged space imaging and lunar robotics · commercial availability
The 2025 NISA datasheet describes onboard image processing and storage, Asp scripting for automated operation, and colour, mono or multispectral and lens customization.
Supports: Rugged space imaging and lunar robotics · technicaldomainslugs
The 2025 NISA datasheet describes onboard image processing and storage, Asp scripting for automated operation, and colour, mono or multispectral and lens customization.
Supports: Rugged space imaging and lunar robotics · core features
NISA’s 2025-04-28 indicative 186-degree configuration has a 4000 by 3000 imager, 64 GB flash or 32 GB high-reliability mode, a 135 g mass and RS-422, USB 2.0 and Ethernet-over-USB interfaces.
Supports: Rugged space imaging and lunar robotics · core features
The 2025 NISA datasheet describes onboard image processing and storage, Asp scripting for automated operation, and colour, mono or multispectral and lens customization.
Supports: Rugged space imaging and lunar robotics · summary
NISA’s 2025-04-28 indicative 186-degree configuration has a 4000 by 3000 imager, 64 GB flash or 32 GB high-reliability mode, a 135 g mass and RS-422, USB 2.0 and Ethernet-over-USB interfaces.
Supports: Rugged space imaging and lunar robotics → Autonomous Patrol and Monitoring
The 2025 NISA datasheet describes onboard image processing and storage, Asp scripting for automated operation, and colour, mono or multispectral and lens customization.
Supports: Rugged space imaging and lunar robotics → Autonomous Patrol and Monitoring
The 2025 NISA datasheet describes onboard image processing and storage, Asp scripting for automated operation, and colour, mono or multispectral and lens customization.
Supports: Rugged space imaging and lunar robotics → Autonomous Patrol and Monitoring
The 2025 NISA datasheet describes onboard image processing and storage, Asp scripting for automated operation, and colour, mono or multispectral and lens customization.
Supports: Rugged space imaging and lunar robotics → Autonomous Patrol and Monitoring
The 2025 NISA datasheet describes onboard image processing and storage, Asp scripting for automated operation, and colour, mono or multispectral and lens customization.
On 15 September 2026 Canadensys announced it is supporting Growcer in a CSA study to conceptually design a deployable controlled-environment agriculture unit for potential future integration into an Inuit-led Nunavut food-security initiative.
On 15 September 2026 Canadensys announced it is supporting Growcer in a CSA study to conceptually design a deployable controlled-environment agriculture unit for potential future integration into an Inuit-led Nunavut food-security initiative.
On 15 September 2026 Canadensys announced it is supporting Growcer in a CSA study to conceptually design a deployable controlled-environment agriculture unit for potential future integration into an Inuit-led Nunavut food-security initiative.
On 15 September 2026 Canadensys announced it is supporting Growcer in a CSA study to conceptually design a deployable controlled-environment agriculture unit for potential future integration into an Inuit-led Nunavut food-security initiative.
Supports: Profile · operating context
Canadensys says it is supporting Growcer on a CSA study for a deployable controlled-environment agriculture concept that could later support an Inuit-led Nunavut food-security initiative. This is conceptual design and two-way technology assessment, not an installed Arctic farm.
Supports: Profile · dual use posture
On 15 September 2026 Canadensys announced it is supporting Growcer in a CSA study to conceptually design a deployable controlled-environment agriculture unit for potential future integration into an Inuit-led Nunavut food-security initiative.
Supports: Profile · operating context
On 15 September 2026 Canadensys announced it is supporting Growcer in a CSA study to conceptually design a deployable controlled-environment agriculture unit for potential future integration into an Inuit-led Nunavut food-security initiative.
On 15 September 2026 Canadensys announced it is supporting Growcer in a CSA study to conceptually design a deployable controlled-environment agriculture unit for potential future integration into an Inuit-led Nunavut food-security initiative.
On 15 September 2026 Canadensys announced it is supporting Growcer in a CSA study to conceptually design a deployable controlled-environment agriculture unit for potential future integration into an Inuit-led Nunavut food-security initiative.
On 15 September 2026 Canadensys announced it is supporting Growcer in a CSA study to conceptually design a deployable controlled-environment agriculture unit for potential future integration into an Inuit-led Nunavut food-security initiative.
On 15 September 2026 Canadensys announced it is supporting Growcer in a CSA study to conceptually design a deployable controlled-environment agriculture unit for potential future integration into an Inuit-led Nunavut food-security initiative.
True North Map derives this first-conversation question from the documented Canadensys Aerospace capability, current evidence and the decision gap that remains.
Supports: Profile · canadian footprint
The official capability material supports the named Space mission systems and robotics offering and the bounded operational description prepared for reviewer consideration.
Canadensys Aerospace's public evidence establishes its current role and offering, but it does not answer every access, configuration, eligibility, maturity or buyer question needed for a first business-development conversation.
Supports: Profile · operating context
The official capability material supports the named Space mission systems and robotics offering and the bounded operational description prepared for reviewer consideration.
Supports: Profile · description
The official company material describes Canadensys Aerospace as a Canadian technology business with the public offering summarized in this candidate.
Supports: Rugged space imaging and lunar robotics · summary
The official capability material supports the named Space mission systems and robotics offering and the bounded operational description prepared for reviewer consideration.
On 14 July 2026 Canadensys announced a program to develop and manufacture tritium-based radioisotope heating units with Canadian Nuclear Laboratories; the announcement supplies no flight qualification, delivered heater or heat-output specification.
On 14 July 2026 Canadensys announced a program to develop and manufacture tritium-based radioisotope heating units with Canadian Nuclear Laboratories; the announcement supplies no flight qualification, delivered heater or heat-output specification.
Supports: Profile · executive relevance summary
Source location: executiveRelevanceSummary
On 14 July 2026 Canadensys announced a program to develop and manufacture tritium-based radioisotope heating units with Canadian Nuclear Laboratories; the announcement supplies no flight qualification, delivered heater or heat-output specification.
Supports: Profile · profileData.portfolioScope
On 14 July 2026 Canadensys announced a program to develop and manufacture tritium-based radioisotope heating units with Canadian Nuclear Laboratories; the announcement supplies no flight qualification, delivered heater or heat-output specification.
On 14 July 2026 Canadensys announced a program to develop and manufacture tritium-based radioisotope heating units with Canadian Nuclear Laboratories; the announcement supplies no flight qualification, delivered heater or heat-output specification.
Supports: Profile · commercial status
On 14 July 2026 Canadensys announced a program to develop and manufacture tritium-based radioisotope heating units with Canadian Nuclear Laboratories; the announcement supplies no flight qualification, delivered heater or heat-output specification.
Supports: Profile · operating context
On 14 July 2026 Canadensys announced a program to develop and manufacture tritium-based radioisotope heating units with Canadian Nuclear Laboratories; the announcement supplies no flight qualification, delivered heater or heat-output specification.
Supports: Profile · operating context
Canadensys announced a programme to develop tritium radioisotope heating units for deep-space missions in collaboration with Canadian Nuclear Laboratories. It is heating-system development; no public flight qualification, licensed delivered unit or power-generation performance is established.
Supports: Thermal-system development collaborator relationship
On 14 July 2026 Canadensys announced a program to develop and manufacture tritium-based radioisotope heating units with Canadian Nuclear Laboratories; the announcement supplies no flight qualification, delivered heater or heat-output specification.
Supports: Thermal-system development collaborator relationship
On 14 July 2026 Canadensys announced a program to develop and manufacture tritium-based radioisotope heating units with Canadian Nuclear Laboratories; the announcement supplies no flight qualification, delivered heater or heat-output specification.
Supports: Thermal-system development collaborator relationship
On 14 July 2026 Canadensys announced a program to develop and manufacture tritium-based radioisotope heating units with Canadian Nuclear Laboratories; the announcement supplies no flight qualification, delivered heater or heat-output specification.
Supports: Thermal-system development collaborator relationship
On 14 July 2026 Canadensys announced a program to develop and manufacture tritium-based radioisotope heating units with Canadian Nuclear Laboratories; the announcement supplies no flight qualification, delivered heater or heat-output specification.
The company identifies itself as Canadensys Aerospace Corporation and develops space systems and advanced vehicles for planetary, orbital and terrestrial environments.
Supports: Profile · description
The company identifies itself as Canadensys Aerospace Corporation and develops space systems and advanced vehicles for planetary, orbital and terrestrial environments.
Canadensys reported delivery of the Lunar Vertex multispectral microscope flight model to Johns Hopkins APL on 12 July 2023; five LED wavelengths are intended to examine lunar-soil texture and composition.
Canadensys reported delivery of the Lunar Vertex multispectral microscope flight model to Johns Hopkins APL on 12 July 2023; five LED wavelengths are intended to examine lunar-soil texture and composition.
Supports: Rugged space imaging and lunar robotics · core features
Canadensys reported delivery of the Lunar Vertex multispectral microscope flight model to Johns Hopkins APL on 12 July 2023; five LED wavelengths are intended to examine lunar-soil texture and composition.
Supports: Rugged space imaging and lunar robotics · maturity
Canadensys reported delivery of the Lunar Vertex multispectral microscope flight model to Johns Hopkins APL on 12 July 2023; five LED wavelengths are intended to examine lunar-soil texture and composition.
The live NISA product page still lists -200 to +70 C survival and dimensions of 50 by 50 by 39 mm with the 186-degree lens; the 2025 datasheet instead gives unspecified extended survival and 50 by 50 by 30 mm body with lens holder.
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Supports: Profile · operating context
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
The live NISA product page still lists -200 to +70 C survival and dimensions of 50 by 50 by 39 mm with the 186-degree lens; the 2025 datasheet instead gives unspecified extended survival and 50 by 50 by 30 mm body with lens holder.
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
The live NISA product page still lists -200 to +70 C survival and dimensions of 50 by 50 by 39 mm with the 186-degree lens; the 2025 datasheet instead gives unspecified extended survival and 50 by 50 by 30 mm body with lens holder.
Supports: Rugged space imaging and lunar robotics · summary
The live NISA product page still lists -200 to +70 C survival and dimensions of 50 by 50 by 39 mm with the 186-degree lens; the 2025 datasheet instead gives unspecified extended survival and 50 by 50 by 30 mm body with lens holder.
Supports: Rugged space imaging and lunar robotics · update child
Compact 12-megapixel radiation-tolerant NISA camera; Low-temperature survival and low-power operation; Onboard storage with serial, USB and Ethernet interfaces; Lunar rover, mobility and payload-integration engineering; Flight-proven lunar surface imaging
Supports: Rugged space imaging and lunar robotics · technicaldomainslugs
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Supports: Rugged space imaging and lunar robotics · update child
Lunar and planetary surface imaging; Spacecraft situational awareness and payload imaging; Remote robotic exploration; Sovereign space-system integration and mission support
Supports: Rugged space imaging and lunar robotics · maturity
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Supports: Rugged space imaging and lunar robotics · core features
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Supports: Rugged space imaging and lunar robotics · capability type
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Supports: Rugged space imaging and lunar robotics · update child
Rugged space imaging, avionics and lunar robotics
Supports: Rugged space imaging and lunar robotics · commercial availability
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Supports: Rugged space imaging and lunar robotics · update child
space imaging; lunar robotics; radiation tolerant; embedded avionics; planetary mobility
Supports: Rugged space imaging and lunar robotics · technicaldomainslugs
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Supports: Rugged space imaging and lunar robotics · technical tags
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Supports: Rugged space imaging and lunar robotics · update child
Canadian space-systems portfolio combining compact radiation-tolerant imaging, onboard storage and interfaces, lunar and planetary mobility, payload integration, and mission engineering with publicly documented lunar flight use.
Supports: Rugged space imaging and lunar robotics · update child
Rugged space imaging and lunar robotics
Supports: Rugged space imaging and lunar robotics · summary
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Supports: Rugged space imaging and lunar robotics · core features
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Supports: Rugged space imaging and lunar robotics · technical tags
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Supports: Rugged space imaging and lunar robotics · technical tags
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Supports: Rugged space imaging and lunar robotics · name
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Supports: Rugged space imaging and lunar robotics · core features
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Supports: Rugged space imaging and lunar robotics · technicaldomainslugs
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Supports: Rugged space imaging and lunar robotics · defence applications
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
Supports: Rugged space imaging and lunar robotics · technology readiness level
Canadensys specifies NISA cameras with 12 MP imaging, 64 GB storage (32 GB high-reliability mode), RS-422/USB interfaces and Ethernet over USB. Operating temperature is -25 to +50 C; -200 to +70 C is survival, not imaging operation. The company describes camera use on IM-1 and other lunar missions; this does not confer flight heritage on every rover or payload.
The January 2021 RAPTOR brochure lists 30 km/h speed, 1000 kg maximum payload, 2700 kg gross and 1700 kg curb weight, 366 by 163 by 120 cm dimensions, and 24 V / 3 kW exportable payload power.
The January 2021 RAPTOR brochure lists 30 km/h speed, 1000 kg maximum payload, 2700 kg gross and 1700 kg curb weight, 366 by 163 by 120 cm dimensions, and 24 V / 3 kW exportable payload power.
Supports: RAPTOR and HAWC ground vehicles · summary
The RAPTOR brochure describes battery operation with an optional diesel generator, CAN-controlled motor controllers and an open payload deck; these are dated configuration options rather than a universal autonomous operating envelope.
Supports: RAPTOR and HAWC ground vehicles · core features
The RAPTOR brochure describes battery operation with an optional diesel generator, CAN-controlled motor controllers and an open payload deck; these are dated configuration options rather than a universal autonomous operating envelope.
Supports: RAPTOR and HAWC ground vehicles · core features
The January 2021 RAPTOR brochure lists 30 km/h speed, 1000 kg maximum payload, 2700 kg gross and 1700 kg curb weight, 366 by 163 by 120 cm dimensions, and 24 V / 3 kW exportable payload power.
Supports: RAPTOR and HAWC ground vehicles · summary
The January 2021 RAPTOR brochure lists 30 km/h speed, 1000 kg maximum payload, 2700 kg gross and 1700 kg curb weight, 366 by 163 by 120 cm dimensions, and 24 V / 3 kW exportable payload power.
Supports: RAPTOR and HAWC ground vehicles · core features
The January 2021 RAPTOR brochure lists 30 km/h speed, 1000 kg maximum payload, 2700 kg gross and 1700 kg curb weight, 366 by 163 by 120 cm dimensions, and 24 V / 3 kW exportable payload power.
CSA identifies the Canadian utility rover as concept development with launch in the 2030s.
Supports: Profile · executive relevance summary
Source location: executiveRelevanceSummary
CSA identifies the Canadian utility rover as concept development with launch in the 2030s.
Supports: Profile · operating context
CSA identifies the lunar utility rover as concept development for launch in the 2030s. July 2025 preparatory-study contracts total CAD 14.6 million across Canadensys, MDA Space and Mission Control over eighteen months; that aggregate is not Canadensys revenue or a final flight-production award.
CSA identifies the lunar utility rover as concept development for launch in the 2030s. July 2025 preparatory-study contracts total CAD 14.6 million across Canadensys, MDA Space and Mission Control over eighteen months; that aggregate is not Canadensys revenue or a final flight-production award.
Supports: Rugged space imaging and lunar robotics · capability type
CSA identifies the Canadian utility rover as concept development with launch in the 2030s.
Supports: Rugged space imaging and lunar robotics · summary
CSA identifies the Canadian utility rover as concept development with launch in the 2030s.
Supports: Rugged space imaging and lunar robotics · commercial availability
CSA identifies the Canadian utility rover as concept development with launch in the 2030s.
Supports: Rugged space imaging and lunar robotics · defence applications
CSA identifies the Canadian utility rover as concept development with launch in the 2030s.
Supports: Rugged space imaging and lunar robotics · core features
CSA identifies the lunar utility rover as concept development for launch in the 2030s. July 2025 preparatory-study contracts total CAD 14.6 million across Canadensys, MDA Space and Mission Control over eighteen months; that aggregate is not Canadensys revenue or a final flight-production award.
Supports: Rugged space imaging and lunar robotics · maturity
CSA identifies the Canadian utility rover as concept development with launch in the 2030s.
Supports: Rugged space imaging and lunar robotics · summary
CSA identifies the lunar utility rover as concept development for launch in the 2030s. July 2025 preparatory-study contracts total CAD 14.6 million across Canadensys, MDA Space and Mission Control over eighteen months; that aggregate is not Canadensys revenue or a final flight-production award.
Supports: Rugged space imaging and lunar robotics · technicaldomainslugs
CSA identifies the Canadian utility rover as concept development with launch in the 2030s.
Supports: Rugged space imaging and lunar robotics · technical tags
CSA identifies the Canadian utility rover as concept development with launch in the 2030s.
Supports: Rugged space imaging and lunar robotics · technicaldomainslugs
CSA identifies the Canadian utility rover as concept development with launch in the 2030s.
Canadensys announced a CSA task authorization on 8 August 2025 to refine plant-growth racks, nutrient delivery, lighting and health monitoring concepts for a lunar-agriculture ground test demonstrator, supported by Guelph and McGill teams.
Supports: Profile · operating context
Canadensys announced a CSA task authorization on 8 August 2025 to refine plant-growth racks, nutrient delivery, lighting and health monitoring concepts for a lunar-agriculture ground test demonstrator, supported by Guelph and McGill teams.
Canadensys announced a CSA task authorization on 8 August 2025 to refine plant-growth racks, nutrient delivery, lighting and health monitoring concepts for a lunar-agriculture ground test demonstrator, supported by Guelph and McGill teams.
Supports: Profile · profileData.portfolioScope
Canadensys announced a CSA task authorization on 8 August 2025 to refine plant-growth racks, nutrient delivery, lighting and health monitoring concepts for a lunar-agriculture ground test demonstrator, supported by Guelph and McGill teams.
Supports: Profile · commercial status
Canadensys announced a CSA task authorization on 8 August 2025 to refine plant-growth racks, nutrient delivery, lighting and health monitoring concepts for a lunar-agriculture ground test demonstrator, supported by Guelph and McGill teams.
Canadensys announced a CSA task authorization on 8 August 2025 to refine plant-growth racks, nutrient delivery, lighting and health monitoring concepts for a lunar-agriculture ground test demonstrator, supported by Guelph and McGill teams.
CSA marks the first Canadian lunar rover project as ended. It says technology and knowledge may contribute to other missions including the separate lunar utility rover; prior planned launch dates are superseded.
CSA marks the first Canadian lunar rover project as ended. It says technology and knowledge may contribute to other missions including the separate lunar utility rover; prior planned launch dates are superseded.
Supports: Rugged space imaging and lunar robotics · summary
CSA marks the first Canadian lunar rover project as ended. It says technology and knowledge may contribute to other missions including the separate lunar utility rover; prior planned launch dates are superseded.
APL’s current Lunar Vertex mission page identifies Canadensys’s multispectral microscope on the Lunar Outpost rover and a launch no earlier than 2026; the page does not establish completed lunar operation.
APL’s current Lunar Vertex mission page identifies Canadensys’s multispectral microscope on the Lunar Outpost rover and a launch no earlier than 2026; the page does not establish completed lunar operation.
APL’s current Lunar Vertex mission page identifies Canadensys’s multispectral microscope on the Lunar Outpost rover and a launch no earlier than 2026; the page does not establish completed lunar operation.
Supports: Rugged space imaging and lunar robotics · maturity
APL’s current Lunar Vertex mission page identifies Canadensys’s multispectral microscope on the Lunar Outpost rover and a launch no earlier than 2026; the page does not establish completed lunar operation.
Supports: Rugged space imaging and lunar robotics · summary
APL’s current Lunar Vertex mission page identifies Canadensys’s multispectral microscope on the Lunar Outpost rover and a launch no earlier than 2026; the page does not establish completed lunar operation.
CSA’s French 24 July 2026 announcement awards Growcer up to C$745,000 to develop a controlled-environment agriculture concept with Inuit enterprise Arctic Fresh; the recipient is Growcer, not Canadensys.
CSA’s French 24 July 2026 announcement awards Growcer up to C$745,000 to develop a controlled-environment agriculture concept with Inuit enterprise Arctic Fresh; the recipient is Growcer, not Canadensys.
CanadaBuys names Canadensys for contract CW2394557 awarded 25 July 2025, with a C$4,724,895 value and 18-month period to 24 January 2027; scope comprises Phase 0 concept studies and an initial critical-technology development option.
Supports: Profile · operating context
CanadaBuys names Canadensys for contract CW2394557 awarded 25 July 2025, with a C$4,724,895 value and 18-month period to 24 January 2027; scope comprises Phase 0 concept studies and an initial critical-technology development option.
Supports: Profile · commercial status
CanadaBuys names Canadensys for contract CW2394557 awarded 25 July 2025, with a C$4,724,895 value and 18-month period to 24 January 2027; scope comprises Phase 0 concept studies and an initial critical-technology development option.
Supports: Profile · legal name
CanadaBuys names Canadensys for contract CW2394557 awarded 25 July 2025, with a C$4,724,895 value and 18-month period to 24 January 2027; scope comprises Phase 0 concept studies and an initial critical-technology development option.
Supports: Profile · canadian footprint
CanadaBuys names Canadensys for contract CW2394557 awarded 25 July 2025, with a C$4,724,895 value and 18-month period to 24 January 2027; scope comprises Phase 0 concept studies and an initial critical-technology development option.
Supports: Rugged space imaging and lunar robotics · core features
CanadaBuys names Canadensys for contract CW2394557 awarded 25 July 2025, with a C$4,724,895 value and 18-month period to 24 January 2027; scope comprises Phase 0 concept studies and an initial critical-technology development option.
ILOA’s live support page confirms a current Canadensys development contract for ILO-1 on the Astrolab FLEX rover and currently expects lunar operation beginning in 2029.
Supports: Profile · commercial status
ILOA’s live support page confirms a current Canadensys development contract for ILO-1 on the Astrolab FLEX rover and currently expects lunar operation beginning in 2029.
Supports: Profile · operating context
ILOA’s live support page confirms a current Canadensys development contract for ILO-1 on the Astrolab FLEX rover and currently expects lunar operation beginning in 2029.
ILOA’s live support page confirms a current Canadensys development contract for ILO-1 on the Astrolab FLEX rover and currently expects lunar operation beginning in 2029.
Supports: Rugged space imaging and lunar robotics · summary
ILOA’s live support page confirms a current Canadensys development contract for ILO-1 on the Astrolab FLEX rover and currently expects lunar operation beginning in 2029.
Supports: Instrument development customer relationship
ILOA’s live support page confirms a current Canadensys development contract for ILO-1 on the Astrolab FLEX rover and currently expects lunar operation beginning in 2029.
The live official Controlled Goods Program record names Canadensys Aerospace Corporation with expiry 31 March 2027; it does not establish a facility security clearance or a site-specific classified-work authorization.
ILOA’s 29 February 2024 mission report identifies Canadensys as ILO-X developer and contractor and confirms return of lunar descent and surface images from its dual-camera payload on Intuitive Machines IM-1.
Supports: Profile · operating context
ILOA’s 29 February 2024 mission report identifies Canadensys as ILO-X developer and contractor and confirms return of lunar descent and surface images from its dual-camera payload on Intuitive Machines IM-1.
Supports: Profile · description
ILOA’s 29 February 2024 mission report identifies Canadensys as ILO-X developer and contractor and confirms return of lunar descent and surface images from its dual-camera payload on Intuitive Machines IM-1.
Supports: Rugged space imaging and lunar robotics · technology readiness level
ILOA’s 29 February 2024 mission report identifies Canadensys as ILO-X developer and contractor and confirms return of lunar descent and surface images from its dual-camera payload on Intuitive Machines IM-1.
Supports: Rugged space imaging and lunar robotics · summary
ILOA’s 29 February 2024 mission report identifies Canadensys as ILO-X developer and contractor and confirms return of lunar descent and surface images from its dual-camera payload on Intuitive Machines IM-1.
Supports: Rugged space imaging and lunar robotics · maturity
ILOA’s 29 February 2024 mission report identifies Canadensys as ILO-X developer and contractor and confirms return of lunar descent and surface images from its dual-camera payload on Intuitive Machines IM-1.
Supports: Instrument development customer relationship
ILOA’s 29 February 2024 mission report identifies Canadensys as ILO-X developer and contractor and confirms return of lunar descent and surface images from its dual-camera payload on Intuitive Machines IM-1.
Chironix lists Canadensys RAPTOR as an available logistics and security platform ready for PilotOS integration, with 1000 kg payload, 30 km/h speed and battery or optional diesel-generator power.
Supports: Profile · executive relevance summary
Source location: executiveRelevanceSummary
Chironix lists Canadensys RAPTOR as an available logistics and security platform ready for PilotOS integration, with 1000 kg payload, 30 km/h speed and battery or optional diesel-generator power.
Chironix lists Canadensys RAPTOR as an available logistics and security platform ready for PilotOS integration, with 1000 kg payload, 30 km/h speed and battery or optional diesel-generator power.
Chironix lists Canadensys RAPTOR as an available logistics and security platform ready for PilotOS integration, with 1000 kg payload, 30 km/h speed and battery or optional diesel-generator power.
Supports: RAPTOR and HAWC ground vehicles · maturity
Chironix lists Canadensys RAPTOR as an available logistics and security platform ready for PilotOS integration, with 1000 kg payload, 30 km/h speed and battery or optional diesel-generator power.
Supports: RAPTOR and HAWC ground vehicles · defence applications
Chironix lists Canadensys RAPTOR as an available logistics and security platform ready for PilotOS integration, with 1000 kg payload, 30 km/h speed and battery or optional diesel-generator power.
Supports: RAPTOR and HAWC ground vehicles · defence applications
Chironix lists Canadensys RAPTOR as an available logistics and security platform ready for PilotOS integration, with 1000 kg payload, 30 km/h speed and battery or optional diesel-generator power.
Supports: RAPTOR and HAWC ground vehicles · summary
Chironix lists Canadensys RAPTOR as an available logistics and security platform ready for PilotOS integration, with 1000 kg payload, 30 km/h speed and battery or optional diesel-generator power.
Supports: RAPTOR and HAWC ground vehicles · commercial availability
Chironix lists Canadensys RAPTOR as an available logistics and security platform ready for PilotOS integration, with 1000 kg payload, 30 km/h speed and battery or optional diesel-generator power.
Supports: RAPTOR and HAWC ground vehicles · core features
Chironix lists Canadensys RAPTOR as an available logistics and security platform ready for PilotOS integration, with 1000 kg payload, 30 km/h speed and battery or optional diesel-generator power.
Supports: RAPTOR and HAWC ground vehicles · core features
Chironix lists Canadensys RAPTOR as an available logistics and security platform ready for PilotOS integration, with 1000 kg payload, 30 km/h speed and battery or optional diesel-generator power.
Canadensys says its facilities support component investigations, design, analysis and test, subsystem qualification, system integration, and environmental qualification and acceptance testing.
Supports: Profile · canadian footprint
Canadensys says its facilities support component investigations, design, analysis and test, subsystem qualification, system integration, and environmental qualification and acceptance testing.
Supports: Profile · canadian footprint
Canadensys lists headquarters at 10 Parr Boulevard, Caledon, Ontario, and a Stratford facility at 753 Ontario Street; it describes over 30,000 square feet across office, laboratory, clean-room and integration space.
Supports: Profile · executive relevance summary
Source location: executiveRelevanceSummary
Canadensys lists headquarters at 10 Parr Boulevard, Caledon, Ontario, and a Stratford facility at 753 Ontario Street; it describes over 30,000 square feet across office, laboratory, clean-room and integration space.
The proactive disclosure for the same CW2394557 lists C$5,173,763.49 and a 11 September 2025 contract date, unlike CanadaBuys’s C$4,724,895 and 25 July date; the inspected records do not reconcile the difference.
ILOA’s current ILO-X mission page says the lander-powered instruments ceased operation on 29 February 2024 after Odysseus lost power; a seven-day operating window does not demonstrate lunar-night survival.
Supports: Rugged space imaging and lunar robotics · summary
ILOA’s current ILO-X mission page says the lander-powered instruments ceased operation on 29 February 2024 after Odysseus lost power; a seven-day operating window does not demonstrate lunar-night survival.
Canadensys announced on 15 September 2025 an ILOA contract to design and build the ILO-1 instrument suite, with lunar-night survival and at least one year of lunar operation as design objectives.
Supports: Instrument development customer relationship
Canadensys announced on 15 September 2025 an ILOA contract to design and build the ILO-1 instrument suite, with lunar-night survival and at least one year of lunar operation as design objectives.
Supports: Instrument development customer relationship
Canadensys announced on 15 September 2025 an ILOA contract to design and build the ILO-1 instrument suite, with lunar-night survival and at least one year of lunar operation as design objectives.
Supports: Instrument development customer relationship
Canadensys announced on 15 September 2025 an ILOA contract to design and build the ILO-1 instrument suite, with lunar-night survival and at least one year of lunar operation as design objectives.
Supports: Instrument development customer relationship
Canadensys announced on 15 September 2025 an ILOA contract to design and build the ILO-1 instrument suite, with lunar-night survival and at least one year of lunar operation as design objectives.
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