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Why this organization matters now
Dated Aug 20, 2026
IEEE Spectrum reported on August 20, 2026 that CRC had shifted emphasis from R-1 toward the larger R-2 design, then projected at 12,000 to 15,000 kilograms to LEO. The report said a fully assembled engine static fire was expected in late 2027 and orbital testing remained several years away.
Source: Minister McGuinty announces strategic investments in sovereign space launch (opens in a new tab)Technologies and services
A closer look at the products, services, operating features, and documented applications that shape the organization’s role.
Development-stage orbital launch vehicles and methalox propulsion
R-series launch vehicles and E-1 methalox engine
What it enables
CRC is developing a shared launch architecture built around the one-engine R-1 technical pathfinder, the seven-engine R-2 medium-lift concept and the E-1 LOX-methane gas-generator engine. Public payload and thrust targets are changing and conflict across current sources; no reviewed record establishes a completed full-engine hot-fire, launch licence, flight or operational launch service.
Evidence strength: ModerateLast reviewed Aug 28, 2026
Operating context
Maturity
Development and pre-flight. SpaceQ reported preliminary turbopump test-article work in July 2026, while IEEE Spectrum reported a full-engine static-fire expectation in late 2027 and orbital testing years away. No reviewed source establishes a completed component test, gas-generator hot-fire, full-engine hot-fire or vehicle flight.
Availability
No reviewed public source establishes a licensed launch site, customer launch-services contract, manifested payload, accepted delivery or operational service. Launch-site arrangements were reported as partnership discussions.
Decision-useful features
- R-1 technical pathfinder powered by one E-1 engine
- R-2 medium-lift concept designed around seven E-1 engines
- Shared propulsion, structures, avionics and ground-system architecture
Technical detail and applications
Documented applications. Sovereign and responsive orbital launch · Defence, civil and commercial satellite deployment
- Mobile R-1 concept with a company-stated call-up target under 96 hours
Public record
Public programs and contracts
Dated participation, delivery roles, partnerships, and disclosed funding provide the operating context behind the profile.
Programs and deployments
Launch the North - Canadian Sovereign Launch Capability Development (R1)
Conditionally selected grant recipient · Launch the North first round
Sponsor or operator: Department of National Defence
FundedMar 16, 2026Organization role. CRC is the recipient under agreement CO5-023. The public record establishes funded development through September 2027; it does not establish a procurement contract, completed prototype, flight, acceptance or operational service.
Program. DND's Launch the North first round funds CRC's R1 project to move a Canadian light-lift launch concept toward prototype and testing, with program-level intent to reach initial operating capability by 2028.
Started Mar 6, 2026 · Ended Sep 30, 2027
Award CO5-023
Prepare the conversation
Questions for a first conversation
Which current R-2 payload, orbit, staging and reuse baseline should a prospective mission planner evaluate?
Current public sources variously state 6,500 kilograms to 500-kilometre LEO, 12,500 kilograms without a reconciled basis, 12,500 kilograms to SSO, and 12,000 to 15,000 kilograms to LEO.
Which E-1 thrust rating and completed component, gas-generator or full-engine test evidence defines the current propulsion baseline?
Company-controlled pages refer to 700, 725 and 750 kilonewtons, while SpaceQ and IEEE Spectrum describe future test milestones rather than published completed results.
Which test-site and launch-site agreements, Transport Canada approvals and launch-licensing milestones are executed rather than under discussion?
SpaceQ reports an undisclosed test site and launch-site partnership discussions; no reviewed public source identifies a CRC launch licence, selected launch site or executed launch-services agreement.
How does the current R-2 emphasis change the deliverables, schedule and light-lift outcome attached to IDEaS agreement CO5-023?
Geography
Toronto, Ontario
The map is centred on Toronto. It does not imply a street address or exact facility location.
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Sources behind this profile
Open the original record, then expand the source details to see which parts of the dossier it informs.
Public sources cited · Facts and assessments kept separate · Human review
Public sources
14
Last reviewed
Aug 28, 2026
Identity and profile
- Open source: Canada Rocket Company R-Series and E-1 product overview (opens in a new tab)
Canada Rocket Company R-Series and E-1 product overview
Canada Rocket Company
Source details
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