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Questions for a first conversation

Which qualification, flight and grant-agreement milestones have been completed for Aurora-8 since conditional selection?
The government selection and company roadmap define a development programme; acceptance milestones determine the move toward an operational service.

Original sources 8 linked records

These records support the organization, its owned capabilities and their reviewed connections. A source count is not a count of independent confirmations.

Reaction Dynamics official capability profile (opens in a new tab)
Reaction Dynamics
Open original source: Reaction Dynamics official capability profile (opens in a new tab)
Source details
Source type: official company product
Supports: Profile · operating context
The official capability material supports the named Space launch vehicles and propulsion offering and the bounded operational description prepared for reviewer consideration.
Supports: Profile · profileData.publicContact.contactPageUrl
The official public contact pathway for Reaction Dynamics is https://reactiondynamics.space/.
Supports: Profile · reviewed questions.reaction-dynamics-first-conversation.question
True North Map derives this first-conversation question from the documented Reaction Dynamics capability, current evidence and the decision gap that remains.
Supports: Profile · canadian footprint
Reaction Dynamics and independent reporting identify the company's current Longueuil, Quebec facility.
Supports: Profile · editorial profile version
Reaction Dynamics has sufficient mapped public evidence for private reviewer consideration of the shared editorial profile template.
Supports: Profile · description
The official company material describes Reaction Dynamics as a Canadian technology business with the public offering summarized in this candidate.
Supports: Profile · reviewed questions.reaction-dynamics-first-conversation.context
Reaction Dynamics'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: Responsive hybrid launch vehicles and propulsion · summary
The official capability material supports the named Space launch vehicles and propulsion offering and the bounded operational description prepared for reviewer consideration.
Company footprint and forward launch schedule (opens in a new tab)
Reaction Dynamics
Open original source: Company footprint and forward launch schedule (opens in a new tab)
Source details
Source type: official company product
Supports: Profile · reviewed questions.reaction-dynamics-configuration-review.id
Reaction Dynamics develops Canadian hybrid launch vehicles from its Longueuil office and workshop, with test facilities in Joliette. Its current company page describes a planned 2026 suborbital demonstration and a 2028 orbital pathfinder, rather than reporting completed launches.
Supports: Profile · reviewed questions.reaction-dynamics-configuration-review.question
Reaction Dynamics develops Canadian hybrid launch vehicles from its Longueuil office and workshop, with test facilities in Joliette. Its current company page describes a planned 2026 suborbital demonstration and a 2028 orbital pathfinder, rather than reporting completed launches.
DND investments in sovereign space launch (opens in a new tab)
National Defence · Mar 16, 2026
Open original source: DND investments in sovereign space launch (opens in a new tab)
Source details
Source type: official policy
Supports: Profile · operating context
National Defence announced on March 16, 2026 that Reaction Dynamics' Aurora-8 Responsive Launch Vehicle was one of three first-round Launch the North projects conditionally approved for C$8.3 million each. This is development and demonstration support under IDEaS, not an operational launch-service purchase.
Reaction Dynamics — Main body / technical sections: Reaction Dynamics defence page describes intended containerized launch deployment and payload up to250kg toSSO. The launch pa (opens in a new tab)
Reaction Dynamics
Open original source: Reaction Dynamics — Main body / technical sections: Reaction Dynamics defence page describes intended containerized launch deployment and payload up to250kg toSSO. The launch pa (opens in a new tab)
Source details
Source type: official company product
Supports: Profile · operating context
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: Responsive hybrid launch vehicles and propulsion · commercial availability
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.

Show 4 more source records

Reaction Dynamics — Main body / technical sections: DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–Septembe (opens in a new tab)
Department of National Defence
Open original source: Reaction Dynamics — Main body / technical sections: DND proactive disclosure records grant CO5-026 of C$8,333,333 for Reaction Dynamics Lab Inc.’s Aurora-8, March6 2026–Septembe (opens in a new tab)
Source details
Source type: official report
Supports: Profile · operating context
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.

Public sources cited · Facts and assessments kept separate · Human review

Reaction Dynamics — Main body / technical sections: Reaction Dynamics currently describes a two-stage Aurora launch architecture with RE-202C engines, standard ESPA or cust

Reaction Dynamics

Open

Source details

Source type: official company product

Supports: Profile · operating context

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: Responsive hybrid launch vehicles and propulsion · commercial availability

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: Responsive hybrid launch vehicles and propulsion · 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: Responsive hybrid launch vehicles and propulsion · 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: Responsive hybrid launch vehicles and propulsion · 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.

Reaction Dynamics

About Reaction Dynamics

Operating context

Canadian footprint

Reaction Dynamics

About Reaction Dynamics

Operating context

Canadian footprint

Technologies & services 1

Responsive hybrid launch vehicles and propulsion

Evidence of maturity

Commercial availability

Core features

Recorded applications

Public record

Reviewed connections

Autonomous Patrol and Monitoring

Questions for a first conversation

Which qualification, flight and grant-agreement milestones have been completed for Aurora-8 since conditional selection?

Original sources 8 linked records

About Reaction Dynamics

Operating context

Canadian footprint

About Reaction Dynamics

Operating context

Canadian footprint

Technologies & services 1

Responsive hybrid launch vehicles and propulsion

Evidence of maturity

Commercial availability

Core features

Recorded applications

Public record

Reviewed connections

Autonomous Patrol and Monitoring

Questions for a first conversation

Which qualification, flight and grant-agreement milestones have been completed for Aurora-8 since conditional selection?

Original sources 8 linked records

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