C6 Launch Systems is a Canadian space-technology developer working on dedicated small-satellite launch integration, electronically steered communications and cryogenic tank-manufacturing processes. Its launch approach combines purchased components with C6 avionics, telemetry, ground interfaces and vehicle integration. A liquid-engine firing at Spaceport America is independently documented for 2021. Canadian Space Agency records also establish a built and tested STARS communications prototype and a later funded laser-joining project for lightweight stainless-steel cryogenic tanks. These records support a technology-development dossier; they do not establish a current commercial orbital launch service.
Operating context
C6 follows a commercial-component integration model. Its proposed vehicle uses Ursa Major Hadley engines and ISISPACE deployer interfaces, with C6 responsible for avionics, telemetry, ground interfaces and integration. C6 reported integrated ignition, throttling, gimbaling and shutdown tests in April 2021; New Mexico Spaceport Authority independently reports a liquid-engine firing and a retained test stand. This establishes ground activity, not orbital qualification.
The launch architecture remains configuration-sensitive: current pages contain both 30 kg and 100 kg payload statements, the April 2021 release used 50 kg, and C6 and its engine supplier publish different thrust ratings. A buyer needs the controlled vehicle baseline, interface data and test report behind a proposed mission. The public users-guide link is still labelled Coming Soon.
Commercial access is also conditional. C6 announced a Brazilian operator licence in 2021, an Alcantara facilities agreement in 2022, non-exclusive satellite launch agreements with Concert and Phoenix, and a five-year, nonbinding HKATG MOU in 2023. These establish historical relationships, not current site access, an executable manifest or funded customer backlog. SaxaVord appears as a letter-of-intent route. A present delivery discussion needs the relevant operator and mission permissions, site agreement, engine export status and funded launch schedule.
Canadian footprint
C6’s current contact page names Strathroy, Ontario as head office. A C6 media kit also describes a Strathroy base and Toronto offices; CSA disclosures list the recipient in Strathroy for the 2019 and 2023 projects and in Toronto for the 2020 STARS project. This supports a Canadian engineering and development footprint, while present headcount, facility capacity and the split of work between locations remain unverified.
The cross-border operating structure matters: C6 describes C6 Sistemas in Brazil as wholly owned, while its US affiliate CLS 7691 LLC bought the Hadley engine used in the Spaceport America integration programme. US testing and Brazilian launch arrangements should not be counted as Canadian launch-site infrastructure.
Toronto, Ontario is the published city-level context for C6 Launch Systems. It does not imply a street address or exact facility location.
C6 merits a technical-development conversation in three distinct areas: integrated smallsat launch systems, electronically steered space communications and cryogenic tank joining. Independent records establish real ground-test activity and CSA-funded development, which makes those engineering functions more assessable than the launch-service marketing alone. Any payload commitment should first resolve configuration, current site and mission permissions, financing and manifest; component conversations should seek the STARS qualification package or cryogenic-process test envelope before assuming commercial readiness.
Interpretation of the public record. Not qualification, endorsement or evidence of buyer interest.
C6 STARS (Space Transmission and Reception System) combines a phased-array antenna and transceiver to steer radio beams electronically toward Earth- and space-based stations. The intended function is a high-performance data link for launch vehicles and nanosatellites without mechanically steering the antenna. CSA’s public project description says C6 designed, built and tested a prototype.
A CAD 71,990 feasibility contribution was followed by agreement 20STDPK21, valued at CAD 383,377, for design improvements, scale-up and laboratory qualification work during June 2020–March 2022. The project title says toward TRL 6; it does not establish completed TRL 6 qualification or a flight-ready commercial product. The reviewed record does not provide a qualified frequency/bandwidth envelope, radiation or environmental test result, flight integration record or current supply commitment.
Evidence of maturity
A built and tested prototype is documented by CSA; the follow-on project was directed toward TRL 6. Achieved qualification and flight heritage are unverified.
Commercial availability
Research and development capability; an orderable STARS product, qualified interface specification and current delivery schedule are not established.
Core features
Electronic beam steering toward Earth- and space-based receiving stations
Phased-array antenna integrated with a transceiver
CSA describes a designed, built and tested prototype
Follow-on funded work targets design improvements, scale-up and laboratory qualification
Recorded applications
Development of communications links for launch vehicles and nanosatellites
Laser-welding process development for cryogenic tanks
Read technical summary
C6’s Advanced Laser Joining Techniques for Cryogenic Compatible Materials project develops laser-welding practices and processes for lightweight, structurally rigid stainless-steel cryogenic tanks. CSA describes the purpose as reducing mass, cost and production time while increasing manufacturing flexibility for small launch vehicles and modern spacecraft. This is a materials and joining-process development function distinct from launch operations.
CSA agreement 22STDPQ05 records CAD 653,660 over February 2023–January 2026, with a November 2023 amendment. The record also identifies prospective applications in cryogenic hydrogen storage for commercial aircraft and prismatic LNG carriers. It does not publish qualified alloy/thickness ranges, leak or cryogenic-cycle results, pressure limits, an accepted flight tank or production throughput; those limits must be established before using the process in a mission-critical structure.
Evidence of maturity
CSA-funded process development is documented through the disclosed January 2026 agreement end date; qualified process limits and accepted hardware are unverified.
Commercial availability
Development programme; no qualified production process, current manufacturing capacity or commercial tank-supply commitment is established by the reviewed evidence.
Core features
Development of laser-joining practices for stainless-steel cryogenic tank structures
C6 develops a dedicated smallsat launch system by integrating commercial components with its own avionics, telemetry, ground controls and vehicle systems. Its published two-stage design uses three Hadley engines on the first stage and one on the second, with ISISPACE-compatible deployer interfaces. The rocket page targets 100 kg to a 600 km Sun-synchronous orbit; other C6 pages retain smaller payload figures, so this is a source-specific design target rather than demonstrated vehicle performance.
The demonstrated evidence is ground integration. C6 reported an April 2021 campaign covering ignition, throttling, gimbaling, shutdown and cold-flow tests. New Mexico Spaceport Authority independently records a liquid-engine firing and retained test-stand infrastructure. These records improve the evidence for actual systems work, but do not establish orbital qualification, accepted payload delivery or current commercial launch availability. Engine and deployer heritage on other companies’ vehicles cannot substitute for C6 vehicle qualification.
Evidence of maturity
Development with an independently documented 2021 liquid-engine ground firing and company-reported integrated tests. No achieved vehicle TRL or orbital qualification is established.
Commercial availability
Proposed launch service. Historical facilities and customer agreements require current confirmation of licensed site access, funding, vehicle configuration and a deliverable manifest.
Public record
Commercial context
Development-stage launch offering and technology R&D. Historic launch agreements are documented, but present launch-slot availability, binding delivery commitments and completed orbital service are unverified.
Financing and disclosed activity
CSA records disclose CAD 71,990 for a 2019 STARS feasibility project, CAD 383,377 for STARS development under agreement 20STDPK21 covering June 2020–March 2022, and CAD 653,660 for advanced laser joining under agreement 22STDPQ05 covering February 2023–January 2026. These are disclosed contribution agreement values for distinct R&D projects, not revenue, cash balances or evidence that all funds were disbursed. The reviewed public investor page supplies no current financing round or cash position.
Reported stage
Technology development with documented prototype and integrated ground-test activity
Ecosystem relationships
Engine supplier and integration-test partner
Ursa Major Technologies
C6 describes a Master Services Agreement for Hadley engines. Its media kit says US affiliate CLS 7691 LLC purchased the test engine and describes planned Ursa engineering support for the Spaceport America integration programme. Supplier engine heritage does not establish C6 vehicle qualification.
Historical engine integration-test site
Spaceport America
New Mexico Spaceport Authority reports C6’s liquid-engine firing in FY2021 Q4 and retention of test-stand infrastructure. This establishes historical ground-test activity; it does not establish a current launch-site agreement or an orbital service from the facility.
Nonbinding launch-services cooperation MOU
Hong Kong Aerospace Technology Group
HKATG’s 14 April 2023 filing describes a five-year MOU with C6 for launch services, reciprocal customer introductions and possible South American launch-facility cooperation. The filing expressly creates no legal rights or obligations; it is not a firm launch order or financing commitment.
Funding and ownership
Government R&D contribution
$71,990
CSA contribution of CAD 71,990 for the 2019 antenna/transceiver feasibility project that preceded STARS development. The agreement starts 29 April 2019; this is a project contribution value, not corporate financing or evidence of full disbursement.
Government R&D contribution
$383,377
CSA agreement 20STDPK21 discloses CAD 383,377 for STARS design enhancements, scale-up and laboratory qualification toward TRL 6. The disclosed agreement covers 26 June 2020–31 March 2022; no achieved TRL 6 or revenue is inferred.
Government R&D contribution
$653,660
CSA agreement 22STDPQ05 discloses CAD 653,660 for Advanced Laser Joining Techniques for Cryogenic Compatible Materials. The current record covers 9 February 2023–31 January 2026 and identifies a 7 November 2023 amendment; this is a project contribution value, not proof of delivered tanks.
Questions for a first conversation
01
Which current site agreement, operator and mission authorisations, engine-export permissions and funded manifest support the next proposed C6 flight?
The public record contains historical Brazilian and SaxaVord arrangements and non-exclusive customer agreements. Their existence does not establish a launch slot that a payload customer can presently rely on.
02
What controlled vehicle configuration and qualification evidence reconcile the published payload and engine-rating differences?
C6 pages contain 30 kg, 50 kg and 100 kg payload claims across different dates; supplier and C6 engine ratings also differ. Ground firing establishes integration work, while mission mass, orbit and interfaces depend on a confirmed configuration.
03
Which STARS test results, radio-band interfaces and environmental qualification support integration into a customer spacecraft?
CSA documents a built and tested phased-array/transceiver prototype and a follow-on project toward TRL 6. Achieved qualification, a current interface specification and commercial supply status are not established.
04
Which material, joint and cryogenic-cycle test results establish the usable tank-manufacturing envelope from the laser-joining project?
The CSA-funded project targets lightweight stainless-steel cryogenic tanks and ran through January 2026 in the disclosed agreement. The reviewed record gives the objective, not accepted tank hardware, qualified process limits or production capacity.
Original sources 20 linked records
These records support the organization, its owned capabilities and their reviewed connections. A source count is not a count of independent confirmations.
The filing says the MOU creates no legal rights or obligations for the parties.
Supports: Profile · operating context
HKATG announced a 14 April 2023 MOU with C6 covering satellite launch services, reciprocal customer introductions and potential South American launch-facility development.
Supports: Profile · operating context
The MOU has an initial five-year term with an automatic one-year extension and a termination mechanism; continued implementation is not established by this filing.
HKATG announced a 14 April 2023 MOU with C6 covering satellite launch services, reciprocal customer introductions and potential South American launch-facility development.
The MOU has an initial five-year term with an automatic one-year extension and a termination mechanism; continued implementation is not established by this filing.
HKATG announced a 14 April 2023 MOU with C6 covering satellite launch services, reciprocal customer introductions and potential South American launch-facility development.
HKATG announced a 14 April 2023 MOU with C6 covering satellite launch services, reciprocal customer introductions and potential South American launch-facility development.
HKATG announced a 14 April 2023 MOU with C6 covering satellite launch services, reciprocal customer introductions and potential South American launch-facility development.
The official capability material supports the named Launch vehicle systems and propulsion offering and the bounded operational description prepared for reviewer consideration.
Supports: Profile · operating context
The official capability material supports the named Launch vehicle systems and propulsion offering and the bounded operational description prepared for reviewer consideration.
True North Map derives this first-conversation question from the documented C6 Launch Systems capability, current evidence and the decision gap that remains.
Supports: Profile · display lead
C6 says its internal work covers systems integration, avionics, telemetry and communications, and fuel-tank design.
Supports: Profile · operating context
C6 markets a planned dedicated smallsat launch service for payloads up to 100 kg, using commercial components and proprietary integration. Its listed spaceport, engine and ground-software partners do not establish a completed orbital launch, a firm launch date or current licensed service availability.
C6 markets a planned dedicated smallsat launch service for payloads up to 100 kg, using commercial components and proprietary integration. Its listed spaceport, engine and ground-software partners do not establish a completed orbital launch, a firm launch date or current licensed service availability.
Supports: Profile · executive relevance summary
Source location: executiveRelevanceSummary
C6 says its internal work covers systems integration, avionics, telemetry and communications, and fuel-tank design.
C6 Launch Systems'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 · profileData.portfolioScope
C6 describes development of a dedicated smallsat launch vehicle using commercial-off-the-shelf components.
Supports: Profile · dual use posture
C6 describes development of a dedicated smallsat launch vehicle using commercial-off-the-shelf components.
Supports: Profile · role descriptor
C6 describes development of a dedicated smallsat launch vehicle using commercial-off-the-shelf components.
Supports: Profile · description
C6 says its internal work covers systems integration, avionics, telemetry and communications, and fuel-tank design.
Supports: Profile · editorial profile version
C6 Launch Systems has sufficient mapped public evidence for private reviewer consideration of the shared editorial profile template.
Supports: Profile · description
The official company material describes C6 Launch Systems as a Canadian technology business with the public offering summarized in this candidate.
Supports: Launch vehicle systems and propulsion · name
C6 markets a planned dedicated smallsat launch service for payloads up to 100 kg, using commercial components and proprietary integration. Its listed spaceport, engine and ground-software partners do not establish a completed orbital launch, a firm launch date or current licensed service availability.
Supports: Launch vehicle systems and propulsion · defence applications
C6 describes development of a dedicated smallsat launch vehicle using commercial-off-the-shelf components.
Supports: Launch vehicle systems and propulsion · summary
C6 markets a planned dedicated smallsat launch service for payloads up to 100 kg, using commercial components and proprietary integration. Its listed spaceport, engine and ground-software partners do not establish a completed orbital launch, a firm launch date or current licensed service availability.
Supports: Launch vehicle systems and propulsion · technical tags
C6 markets a planned dedicated smallsat launch service for payloads up to 100 kg, using commercial components and proprietary integration. Its listed spaceport, engine and ground-software partners do not establish a completed orbital launch, a firm launch date or current licensed service availability.
Supports: Launch vehicle systems and propulsion · commercial availability
C6 markets a planned dedicated smallsat launch service for payloads up to 100 kg, using commercial components and proprietary integration. Its listed spaceport, engine and ground-software partners do not establish a completed orbital launch, a firm launch date or current licensed service availability.
Supports: Launch vehicle systems and propulsion · technicaldomainslugs
C6 markets a planned dedicated smallsat launch service for payloads up to 100 kg, using commercial components and proprietary integration. Its listed spaceport, engine and ground-software partners do not establish a completed orbital launch, a firm launch date or current licensed service availability.
Supports: Launch vehicle systems and propulsion · technicaldomainslugs
C6 describes development of a dedicated smallsat launch vehicle using commercial-off-the-shelf components.
Supports: Launch vehicle systems and propulsion · technical tags
C6 says its internal work covers systems integration, avionics, telemetry and communications, and fuel-tank design.
Supports: Launch vehicle systems and propulsion · defence applications
C6 markets a planned dedicated smallsat launch service for payloads up to 100 kg, using commercial components and proprietary integration. Its listed spaceport, engine and ground-software partners do not establish a completed orbital launch, a firm launch date or current licensed service availability.
Supports: Launch vehicle systems and propulsion · summary
C6 says its internal work covers systems integration, avionics, telemetry and communications, and fuel-tank design.
Supports: Launch vehicle systems and propulsion · capability type
C6 markets a planned dedicated smallsat launch service for payloads up to 100 kg, using commercial components and proprietary integration. Its listed spaceport, engine and ground-software partners do not establish a completed orbital launch, a firm launch date or current licensed service availability.
Supports: Launch vehicle systems and propulsion · core features
C6 markets a planned dedicated smallsat launch service for payloads up to 100 kg, using commercial components and proprietary integration. Its listed spaceport, engine and ground-software partners do not establish a completed orbital launch, a firm launch date or current licensed service availability.
Supports: Launch vehicle systems and propulsion · technology readiness level
C6 markets a planned dedicated smallsat launch service for payloads up to 100 kg, using commercial components and proprietary integration. Its listed spaceport, engine and ground-software partners do not establish a completed orbital launch, a firm launch date or current licensed service availability.
Supports: Launch vehicle systems and propulsion · name
C6 describes development of a dedicated smallsat launch vehicle using commercial-off-the-shelf components.
Supports: Launch vehicle systems and propulsion · maturity
C6 markets a planned dedicated smallsat launch service for payloads up to 100 kg, using commercial components and proprietary integration. Its listed spaceport, engine and ground-software partners do not establish a completed orbital launch, a firm launch date or current licensed service availability.
Supports: Launch vehicle systems and propulsion · technicaldomainslugs
C6 describes development of a dedicated smallsat launch vehicle using commercial-off-the-shelf components.
Supports: Launch vehicle systems and propulsion · summary
The official capability material supports the named Launch vehicle systems and propulsion offering and the bounded operational description prepared for reviewer consideration.
Supports: Launch vehicle systems and propulsion · capability type
C6 says its internal work covers systems integration, avionics, telemetry and communications, and fuel-tank design.
Supports: Launch vehicle systems and propulsion · technical tags
C6 markets a planned dedicated smallsat launch service for payloads up to 100 kg, using commercial components and proprietary integration. Its listed spaceport, engine and ground-software partners do not establish a completed orbital launch, a firm launch date or current licensed service availability.
Supports: Launch vehicle systems and propulsion · technicaldomainslugs
C6 markets a planned dedicated smallsat launch service for payloads up to 100 kg, using commercial components and proprietary integration. Its listed spaceport, engine and ground-software partners do not establish a completed orbital launch, a firm launch date or current licensed service availability.
Supports: Launch vehicle systems and propulsion · technical tags
C6 describes development of a dedicated smallsat launch vehicle using commercial-off-the-shelf components.
Supports: Profile · canadian footprint
The CSA contribution record identifies C6 Launch Systems, Corporation in Strathroy, Ontario.
Supports: C6 STARS space communications development · summary
The 2019 project studied a low-cost antenna and transceiver that electronically steers radio signals without physically moving the antenna.
Supports: C6 STARS space communications development · summary
CSA records a CAD 71,990 contribution to C6 Launch Systems, Corporation starting 29 April 2019.
Supports: Government R&D contribution funding event
CSA records a CAD 71,990 contribution to C6 Launch Systems, Corporation starting 29 April 2019.
Supports: Government R&D contribution funding event
CSA records a CAD 71,990 contribution to C6 Launch Systems, Corporation starting 29 April 2019.
Supports: Government R&D contribution funding event
CSA records a CAD 71,990 contribution to C6 Launch Systems, Corporation starting 29 April 2019.
Supports: Government R&D contribution funding event
CSA records a CAD 71,990 contribution to C6 Launch Systems, Corporation starting 29 April 2019.
Supports: Government R&D contribution funding event
CSA records a CAD 71,990 contribution to C6 Launch Systems, Corporation starting 29 April 2019.
The project aims to develop laser-welding practices and processes for lightweight, structurally rigid stainless-steel cryogenic-storage tanks.
Supports: Profile · dual use posture
CSA identifies small launch vehicles and modern spacecraft as motivating applications for lightweight tank manufacturing.
Supports: Profile · profileData.portfolioScope
The project aims to develop laser-welding practices and processes for lightweight, structurally rigid stainless-steel cryogenic-storage tanks.
Supports: Profile · disclosed financing summary
CSA records a CAD 653,660 contribution under agreement 22STDPQ05 for Advanced Laser Joining Techniques for Cryogenic Compatible Materials.
Supports: Profile · dual use posture
CSA identifies prospective cryogenic-hydrogen storage for commercial aircraft and prismatic LNG carriers as terrestrial applications of the manufacturing technology.
Supports: Profile · disclosed financing summary
The agreement runs from 9 February 2023 to 31 January 2026; the current record lists an amendment dated 7 November 2023.
Supports: Profile · canadian footprint
The laser-joining contribution identifies C6 Launch Systems in Strathroy, Ontario.
Supports: Profile · executive relevance summary
Source location: executiveRelevanceSummary
The project aims to develop laser-welding practices and processes for lightweight, structurally rigid stainless-steel cryogenic-storage tanks.
Supports: Cryogenic-compatible laser joining development · name
The project aims to develop laser-welding practices and processes for lightweight, structurally rigid stainless-steel cryogenic-storage tanks.
Supports: Cryogenic-compatible laser joining development · capability type
The project aims to develop laser-welding practices and processes for lightweight, structurally rigid stainless-steel cryogenic-storage tanks.
Supports: Cryogenic-compatible laser joining development · defence applications
CSA identifies prospective cryogenic-hydrogen storage for commercial aircraft and prismatic LNG carriers as terrestrial applications of the manufacturing technology.
Supports: Cryogenic-compatible laser joining development · core features
CSA describes reducing production time as an objective of the cryogenic laser-joining development.
Supports: Cryogenic-compatible laser joining development · summary
The agreement runs from 9 February 2023 to 31 January 2026; the current record lists an amendment dated 7 November 2023.
Supports: Cryogenic-compatible laser joining development · summary
CSA identifies small launch vehicles and modern spacecraft as motivating applications for lightweight tank manufacturing.
Supports: Cryogenic-compatible laser joining development · summary
CSA identifies prospective cryogenic-hydrogen storage for commercial aircraft and prismatic LNG carriers as terrestrial applications of the manufacturing technology.
Supports: Cryogenic-compatible laser joining development · technical tags
The project aims to develop laser-welding practices and processes for lightweight, structurally rigid stainless-steel cryogenic-storage tanks.
Supports: Cryogenic-compatible laser joining development · summary
The record describes an R&D objective; it provides no completed qualification result, measured production rate or accepted commercial tank delivery.
Supports: Cryogenic-compatible laser joining development · technicaldomainslugs
The project aims to develop laser-welding practices and processes for lightweight, structurally rigid stainless-steel cryogenic-storage tanks.
Supports: Cryogenic-compatible laser joining development · slug
The project aims to develop laser-welding practices and processes for lightweight, structurally rigid stainless-steel cryogenic-storage tanks.
Supports: Cryogenic-compatible laser joining development · core features
CSA describes increased design flexibility and agility as an objective of the cryogenic laser-joining development.
Supports: Cryogenic-compatible laser joining development · technicaldomainslugs
CSA identifies small launch vehicles and modern spacecraft as motivating applications for lightweight tank manufacturing.
Supports: Cryogenic-compatible laser joining development · defence applications
CSA identifies small launch vehicles and modern spacecraft as motivating applications for lightweight tank manufacturing.
Supports: Cryogenic-compatible laser joining development · core features
CSA describes cost reduction as an objective of the cryogenic laser-joining development.
Supports: Cryogenic-compatible laser joining development · maturity
The record describes an R&D objective; it provides no completed qualification result, measured production rate or accepted commercial tank delivery.
Supports: Cryogenic-compatible laser joining development · core features
The project aims to develop laser-welding practices and processes for lightweight, structurally rigid stainless-steel cryogenic-storage tanks.
Supports: Cryogenic-compatible laser joining development · summary
CSA describes cost reduction as an objective of the cryogenic laser-joining development.
Supports: Cryogenic-compatible laser joining development · maturity
The agreement runs from 9 February 2023 to 31 January 2026; the current record lists an amendment dated 7 November 2023.
Supports: Cryogenic-compatible laser joining development · summary
CSA describes increased design flexibility and agility as an objective of the cryogenic laser-joining development.
Supports: Cryogenic-compatible laser joining development · defence applications
CSA identifies prospective cryogenic-hydrogen storage for commercial aircraft and prismatic LNG carriers as terrestrial applications of the manufacturing technology.
Supports: Cryogenic-compatible laser joining development · technology readiness level
The record describes an R&D objective; it provides no completed qualification result, measured production rate or accepted commercial tank delivery.
Supports: Cryogenic-compatible laser joining development · summary
CSA describes reducing production time as an objective of the cryogenic laser-joining development.
Supports: Cryogenic-compatible laser joining development · summary
The project aims to develop laser-welding practices and processes for lightweight, structurally rigid stainless-steel cryogenic-storage tanks.
Supports: Cryogenic-compatible laser joining development · technical tags
The project aims to develop laser-welding practices and processes for lightweight, structurally rigid stainless-steel cryogenic-storage tanks.
Supports: Cryogenic-compatible laser joining development · technical tags
The project aims to develop laser-welding practices and processes for lightweight, structurally rigid stainless-steel cryogenic-storage tanks.
Supports: Cryogenic-compatible laser joining development · core features
The project aims to develop laser-welding practices and processes for lightweight, structurally rigid stainless-steel cryogenic-storage tanks.
Supports: Cryogenic-compatible laser joining development · summary
CSA records a CAD 653,660 contribution under agreement 22STDPQ05 for Advanced Laser Joining Techniques for Cryogenic Compatible Materials.
Supports: Cryogenic-compatible laser joining development · commercial availability
The record describes an R&D objective; it provides no completed qualification result, measured production rate or accepted commercial tank delivery.
Supports: Cryogenic-compatible laser joining development · technical tags
The project aims to develop laser-welding practices and processes for lightweight, structurally rigid stainless-steel cryogenic-storage tanks.
Supports: Government R&D contribution funding event
The agreement runs from 9 February 2023 to 31 January 2026; the current record lists an amendment dated 7 November 2023.
Supports: Government R&D contribution funding event
The project aims to develop laser-welding practices and processes for lightweight, structurally rigid stainless-steel cryogenic-storage tanks.
Supports: Government R&D contribution funding event
CSA records a CAD 653,660 contribution under agreement 22STDPQ05 for Advanced Laser Joining Techniques for Cryogenic Compatible Materials.
Supports: Government R&D contribution funding event
CSA records a CAD 653,660 contribution under agreement 22STDPQ05 for Advanced Laser Joining Techniques for Cryogenic Compatible Materials.
Supports: Government R&D contribution funding event
CSA records a CAD 653,660 contribution under agreement 22STDPQ05 for Advanced Laser Joining Techniques for Cryogenic Compatible Materials.
Supports: Government R&D contribution funding event
CSA records a CAD 653,660 contribution under agreement 22STDPQ05 for Advanced Laser Joining Techniques for Cryogenic Compatible Materials.
Supports: Government R&D contribution funding event
CSA records a CAD 653,660 contribution under agreement 22STDPQ05 for Advanced Laser Joining Techniques for Cryogenic Compatible Materials.
C6 reports a Master Services Agreement with Ursa Major Technologies for use of the Hadley engine.
Supports: Profile · operating context
C6 describes commercial-component integration, including an ISISpace deployment system and planned use of the Ursa Major Hadley engine. These are design and supplier choices; the current page does not document a completed orbital mission or an accepted commercial payload delivery.
Supports: Profile · operating context
C6 describes a universal mounting plate above stage two accepting ISISpace QuadPack, DuoPack, ISIPODS, custom or externally sourced deployers.
C6 describes commercial-component integration, including an ISISpace deployment system and planned use of the Ursa Major Hadley engine. These are design and supplier choices; the current page does not document a completed orbital mission or an accepted commercial payload delivery.
C6 describes commercial-component integration, including an ISISpace deployment system and planned use of the Ursa Major Hadley engine. These are design and supplier choices; the current page does not document a completed orbital mission or an accepted commercial payload delivery.
C6 describes commercial-component integration, including an ISISpace deployment system and planned use of the Ursa Major Hadley engine. These are design and supplier choices; the current page does not document a completed orbital mission or an accepted commercial payload delivery.
C6 describes commercial-component integration, including an ISISpace deployment system and planned use of the Ursa Major Hadley engine. These are design and supplier choices; the current page does not document a completed orbital mission or an accepted commercial payload delivery.
Supports: Launch vehicle systems and propulsion · core features
The rocket page specifies a design diameter of 1 metre.
Supports: Launch vehicle systems and propulsion · summary
The rocket page specifies two stages, with three engines on the booster and one on the second stage.
Supports: Launch vehicle systems and propulsion · core features
C6 describes a universal mounting plate above stage two accepting ISISpace QuadPack, DuoPack, ISIPODS, custom or externally sourced deployers.
Supports: Launch vehicle systems and propulsion · summary
The rocket page specifies a design payload of 100 kg to a 600 km Sun-synchronous orbit.
Supports: Launch vehicle systems and propulsion · core features
C6 specifies payload volume up to 16U plus deployer.
Supports: Launch vehicle systems and propulsion · core features
The rocket page specifies a design height of 13 metres.
Supports: Launch vehicle systems and propulsion · core features
C6 specifies liquid oxygen and kerosene/RP-1 for the Hadley engine.
Supports: Launch vehicle systems and propulsion · summary
C6 describes a universal mounting plate above stage two accepting ISISpace QuadPack, DuoPack, ISIPODS, custom or externally sourced deployers.
Supports: Launch vehicle systems and propulsion · core features
The rocket page specifies a design payload of 100 kg to a 600 km Sun-synchronous orbit.
Supports: Launch vehicle systems and propulsion · technical tags
C6 specifies liquid oxygen and kerosene/RP-1 for the Hadley engine.
Supports: Launch vehicle systems and propulsion · core features
The rocket page specifies two stages, with three engines on the booster and one on the second stage.
Supports: Launch vehicle systems and propulsion · summary
C6 describes commercial-component integration, including an ISISpace deployment system and planned use of the Ursa Major Hadley engine. These are design and supplier choices; the current page does not document a completed orbital mission or an accepted commercial payload delivery.
Supports: Launch vehicle systems and propulsion · technical tags
C6 describes a universal mounting plate above stage two accepting ISISpace QuadPack, DuoPack, ISIPODS, custom or externally sourced deployers.
Supports: Launch vehicle systems and propulsion · core features
C6 describes commercial-component integration, including an ISISpace deployment system and planned use of the Ursa Major Hadley engine. These are design and supplier choices; the current page does not document a completed orbital mission or an accepted commercial payload delivery.
Supports: Launch vehicle systems and propulsion · core features
C6 lists each Hadley engine at 20 kN / 4,500 lbf sea-level thrust.
Supports: Engine supplier and integration-test partner relationship
C6 reports a Master Services Agreement with Ursa Major Technologies for use of the Hadley engine.
Supports: Engine supplier and integration-test partner relationship
C6 reports a Master Services Agreement with Ursa Major Technologies for use of the Hadley engine.
Supports: Engine supplier and integration-test partner relationship
C6 reports a Master Services Agreement with Ursa Major Technologies for use of the Hadley engine.
Supports: Engine supplier and integration-test partner relationship
C6 reports a Master Services Agreement with Ursa Major Technologies for use of the Hadley engine.
The inspected investor page offers an investor-presentation request and describes OEM-style integration, without a named financing round, amount or cash position.
Spaceport America independently documents C6 installing a rocket-engine test stand in March 2021 for integration testing. It corroborates historical ground-test activity by the Canadian company, not orbital launch qualification or a 2026 launch manifest.
Spaceport America independently documents C6 installing a rocket-engine test stand in March 2021 for integration testing. It corroborates historical ground-test activity by the Canadian company, not orbital launch qualification or a 2026 launch manifest.
Supports: Launch vehicle systems and propulsion · core features
Spaceport America independently documents C6 installing a rocket-engine test stand in March 2021 for integration testing. It corroborates historical ground-test activity by the Canadian company, not orbital launch qualification or a 2026 launch manifest.
Supports: Launch vehicle systems and propulsion · summary
Spaceport America independently documents C6 installing a rocket-engine test stand in March 2021 for integration testing. It corroborates historical ground-test activity by the Canadian company, not orbital launch qualification or a 2026 launch manifest.
Supports: Launch vehicle systems and propulsion · summary
ISISPACE describes qualified flight heritage for its deployers across named launch vehicles including Falcon9, PSLV, Vega and H3; it does not list C6 in the inspected heritage list.
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Continue through related organizations, reviewed mission and Defence need connections, programme pathways, and explicitly linked intelligence. Similarity results describe shared areas of work, not partnerships or endorsements.
Organizations
Profiles that provide the strongest reviewed or discovery-led continuation.
