Reaction Dynamics is developing Aurora hybrid-propulsion launch vehicles and containerized ground-support concepts. DND grant CO5-026 records C$8,333,333 for Aurora-8 research from March 2026 to September 2027, advancing a programme aimed at Canadian light-launch capability by 2028. The current design describes a two-stage vehicle, standard or custom payload interfaces and restartable upper-stage intent. Its site gives 250 kg to sun-synchronous orbit and approximately 200 kg to LEO without reconciling configurations; these are supplier design figures, not demonstrated payload performance.
Technical detail
Core features
Aurora two-stage hybrid launch-vehicle development
Standard ESPA or custom payload-interface design options
Containerized ground-support and deployment concept
DND Aurora-8 R&D grant through September 2027
Hybrid propulsion
Small launch vehicle
Responsive space
Suborbital
Orbital launch
Use & integration
Recorded applications
Responsive small-satellite launch
Suborbital technology demonstration
Polar and sun-synchronous mission support
Distributed launch campaign concepts
These describe the reviewed application scope, not confirmed deployments, released requirements or procurement eligibility.
Evidence of maturity
Funded vehicle and propulsion development. A disclosed grant and stated programme objective establish support and intent, not completed orbital flight or payload-delivery acceptance.
Commercial availability
Engagement concerns development and future launch services. Confirm vehicle configuration, payload/orbit assumptions, qualification evidence and mission schedule before treating advertised performance as available.
Integration and verification
Readiness
A technology readiness level is not established by the reviewed public sources.
The publicly described Space launch vehicles and propulsion 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 6 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.
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · summary
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · name
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · technicaldomainslugs
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · defence applications
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · defence applications
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · technicaldomainslugs
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · maturity
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · commercial availability
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · defence applications
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · technical tags
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · technology readiness level
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · technical tags
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · technicaldomainslugs
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · technical tags
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · capability type
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · technical tags
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · core features
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Capability · defence applications
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Mission area · Autonomous Patrol and Monitoring
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Mission area · Autonomous Patrol and Monitoring
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Mission area · Autonomous Patrol and Monitoring
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Supports: Mission area · Autonomous Patrol and Monitoring
DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–September30 2027. It supports R&D toward Canadian launch capability; the wider programme aims for initial light-launch capability by2028, not proof this vehicle has flown.
Two-stage Aurora launch-vehicle architecture; Hybrid propulsion using hydrogen peroxide and solid polymer fuel; Containerized transport and ground-support concept; Restartable upper-stage propulsion; Suborbital and orbital demonstration roadmap
Supports: Capability · update child
hybrid propulsion; small launch vehicle; responsive space; suborbital; orbital launch
Reaction Dynamics defence page describes intended containerized launch deployment and payload up to250kg toSSO. The launch page also gives approximately200kg toLEO; configuration and mission assumptions remain unresolved, so neither should be presented as an achieved payload demonstration.
Supports: Capability · core features
Reaction Dynamics defence page describes intended containerized launch deployment and payload up to250kg toSSO. The launch page also gives approximately200kg toLEO; configuration and mission assumptions remain unresolved, so neither should be presented as an achieved payload demonstration.
Reaction Dynamics July1 2026 discussion positions sovereign launch as infrastructure and refers to its selection in Launch the North. It sets intended rapid-deployment use cases rather than announcing an orbital mission or completed vehicle acceptance.
Reaction Dynamics currently describes a two-stage Aurora launch architecture with RE-202C engines, standard ESPA or customized payload interfaces and multiple-restart upper-stage intent. These are vehicle design claims, not completed flight acceptance. The page itself lists250kg toSSO and~200kg toLEO, leaving performance/configuration reconciliation necessary.
Public sources cited · Facts and assessments kept separate · Human review
Canadian hybrid-propulsion developer advancing the two-stage Aurora small launch vehicle, containerized ground support, restartable upper-stage propulsion, and suborbital-to-orbital demonstrations for responsive space access.
Supports: Capability · update child
Responsive hybrid launch vehicles and propulsion
Supports: Capability · summary
Reaction Dynamics defence page describes intended containerized launch deployment and payload up to250kg toSSO. The launch page also gives approximately200kg toLEO; configuration and mission assumptions remain unresolved, so neither should be presented as an achieved payload demonstration.
Supports: Capability · core features
Reaction Dynamics currently describes a two-stage Aurora launch architecture with RE-202C engines, standard ESPA or customized payload interfaces and multiple-restart upper-stage intent. These are vehicle design claims, not completed flight acceptance. The page itself lists250kg toSSO and~200kg toLEO, leaving performance/configuration reconciliation necessary.
Supports: Capability · core features
Reaction Dynamics currently describes a two-stage Aurora launch architecture with RE-202C engines, standard ESPA or customized payload interfaces and multiple-restart upper-stage intent. These are vehicle design claims, not completed flight acceptance. The page itself lists250kg toSSO and~200kg toLEO, leaving performance/configuration reconciliation necessary.
Supports: Capability · summary
Reaction Dynamics currently describes a two-stage Aurora launch architecture with RE-202C engines, standard ESPA or customized payload interfaces and multiple-restart upper-stage intent. These are vehicle design claims, not completed flight acceptance. The page itself lists250kg toSSO and~200kg toLEO, leaving performance/configuration reconciliation necessary.
The official capability material supports the named Space launch vehicles and propulsion offering and the bounded operational description prepared for reviewer consideration.
