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.
Technical detail
Core features
12 MP NISA imaging; 64 GB flash or 32 GB high-reliability mode in the April 2025 indicative configuration
RS-422, USB 2.0 and Ethernet-over-USB data interfaces
Onboard image processing, storage and Asp scripting for automated acquisition
-25 to +50 C operation; extended survival requires configuration-specific confirmation
Lunar Vertex multispectral microscopy uses five LED wavelengths to examine soil texture and composition
Utility-rover Phase 0 and technology development, separate from the ended first lunar rover project
Space and earth observation
Sensing and isr
Aerospace and mobility
Use & integration
Recorded applications
Spacecraft imaging and mission monitoring
Lunar scientific instruments and planetary mobility engineering
These describe the reviewed application scope, not confirmed deployments, released requirements or procurement eligibility.
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.
Integration and verification
Readiness
A technology readiness level is not established by the reviewed public sources.
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.
This is a reviewed public-source assessment. It is not procurement eligibility, endorsement, customer interest, or classified demand.
Original sources 13 linked records
These records support this capability and its published Mission area and Defence need connections. A source count is not a count of independent confirmations.
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 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: Capability · 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: Capability · 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: Capability · update child
Lunar and planetary surface imaging; Spacecraft situational awareness and payload imaging; Remote robotic exploration; Sovereign space-system integration and mission support
Supports: Capability · 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.
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: Capability · 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 capability material supports the named Space mission systems and robotics offering and the bounded operational description prepared for reviewer consideration.
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: Capability · 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: Capability · update child
Rugged space imaging, avionics and lunar robotics
Supports: Capability · 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: Capability · update child
space imaging; lunar robotics; radiation tolerant; embedded avionics; planetary mobility
Supports: Capability · 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: Capability · 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: Capability · 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: Capability · update child
Rugged space imaging and lunar robotics
Supports: Capability · 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: Capability · 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: Capability · 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: Capability · 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: Capability · 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: Capability · 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: Capability · 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: Capability · 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: Capability · 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.
Supports: Capability · commercial availability
CSA identifies the Canadian utility rover as concept development with launch in the 2030s.
Supports: Capability · defence applications
CSA identifies the Canadian utility rover as concept development with launch in the 2030s.
Supports: Capability · 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: Capability · maturity
CSA identifies the Canadian utility rover as concept development with launch in the 2030s.
Supports: Capability · 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: Capability · technicaldomainslugs
CSA identifies the Canadian utility rover as concept development with launch in the 2030s.
Supports: Capability · technical tags
CSA identifies the Canadian utility rover as concept development with launch in the 2030s.
Supports: Capability · technicaldomainslugs
CSA identifies the Canadian utility rover as concept development with launch in the 2030s.
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: Capability · 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 April 2025 NISA datasheet offers stock or customized cameras for customer requirements, with image, lens, thermal-management, housing, software and integration options.
Supports: Capability · 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: Capability · 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: Capability · 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: Capability · 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: Capability · 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: Capability · 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: Capability · 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: Capability · 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: Capability · 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: Capability · 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: Capability · 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: Capability · 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: Capability · 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: Capability · 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: Capability · 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: Mission area · 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: Mission area · 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: Mission area · 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: Mission area · 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.
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.
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: Capability · 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 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.
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: Capability · 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: Capability · 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.
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.
