Jobs at Canada Rocket Company

Lead Canada Rocket Company’s manufacturing and process strategy for launch-vehicle hardware. Establish in-house and supplier capabilities, qualify materials and fabrication processes, develop documentation and process controls, and lead design-for-manufacture reviews. Manage tooling, industrialization, make-versus-buy decisions, supplier qualification, non-conformances, failure analysis, and production scaling while coordinating with engineering, operations, supply chain, suppliers, and executives.

Open application for candidates interested in operations roles. Applicants should submit a resume and describe their passions, preferred work, and how their background could contribute. The company will contact applicants when a suitable opportunity becomes available.

Lead the flight software organization for an orbital launch vehicle, owning architecture, development, verification, operations, and flight-critical software standards. Build and mentor the team, develop embedded software across RTOS, GPOS, FPGA, and bare-metal environments, integrate with avionics, implement GNC algorithms, and oversee testing, configuration control, code reviews, and anomaly resolution.

This is an open application for engineering candidates. Applicants should submit a resume and describe their passions, preferred work, and potential contributions. The company will contact candidates when a suitable engineering opportunity becomes available.

Own detailed CAD models, assemblies, production drawings, GD&T, tolerance stack-ups, and configuration control for rocket turbopump hardware. Translate engineering analysis into inspectable manufacturing requirements, improve designs for manufacturability, and collaborate with suppliers, machinists, quality teams, and inspectors through release, first-article inspection, testing, and nonconformity dispositioning.

Analyze rocket vehicle fluid systems, cryogenic propellant operations, aerodynamics, aerothermal environments, venting, tank pressurization, and CFD models across ascent and re-entry. Develop analysis codes, aerodynamic databases, and system-level fluid models; support vehicle design trades, testing, flight campaigns, anomaly investigations, and root-cause analysis for an orbital launch vehicle.

Own the technical baseline and integrated execution of test and launch infrastructure from design through construction and commissioning. Manage third-party engineering firms, requirements, specifications, design reviews, schedules, budgets, vendor technical evaluations, change control, constructability, RFIs, and commissioning acceptance. Coordinate engineering, procurement, construction, and facilities teams while serving as the program’s engineering authority.

Manage day-to-day accounting operations, including general ledger, month-end close, financial reporting, accounts payable, treasury, payroll accounting, cost accounting, tax coordination, SR&ED claims, and grant reporting. Lead the transition from outsourced accounting to in-house processes, establish internal controls, implement procure-to-pay and ERP systems, deploy AI-enabled finance workflows, and oversee multi-currency cash management.

Lead end-to-end fluidic design and analysis of cryogenic pumps, hot-side turbines, secondary flow circuits, and axial thrust balancing systems for a rocket engine. Define geometries, run steady and transient multiphase CFD, predict performance across operating maps, develop preliminary design tools, correlate analyses with test data, and support instrumentation, validation, manufacturing, mechanical design, and configuration-controlled engineering reviews.

Own the full lifecycle design of high-reliability electrical hardware for launch vehicles, including architectures, schematics, PCB layout, prototyping, debugging, integration, environmental testing, production support, and failure investigations. Establish scalable electrical design processes and documentation, develop digital, power, and analog circuits, and help build the future electrical engineering team.

Design and develop launch vehicle structural hardware, including tanks, interstages, and integrated assemblies, from concept through manufacturing, testing, and flight integration. Create CAD models, drawings, interfaces, and release packages; perform structural, thermal, vibration, tolerance, and fit-up analyses using calculations and FEA. Collaborate with propulsion, fluids, avionics, manufacturing, integration, and test teams to deliver producible, reliable hardware. A current P.Eng. license is required to hold the Engineer title.

Design and develop mechanical hardware and integrated assemblies for the E1 rocket engine, owning systems from concept through manufacturing, testing, iteration, and flight integration. Create CAD models, drawings, interface definitions, and release packages; perform structural, thermal, vibration, tolerance, and fit-up analyses; and drive packaging, manufacturability, assembly, supplier coordination, and cross-functional integration with propulsion, fluids, avionics, structures, manufacturing, and test teams.

Own propulsion component development from requirements and first-principles design through detailed engineering, manufacturing, component testing, and flight qualification. Design valves, regulators, igniters, piping, flex lines, TVC actuators, thrusters, and related hardware. Create CAD models and drawings, perform engineering analyses, make design-for-manufacture decisions, collaborate cross-functionally, support test planning and instrumentation, and analyze post-test data.

Leads the propulsion and vehicle fluid systems organization for a medium-lift launch vehicle. Responsibilities include setting technical architecture, driving design through flight and reuse, managing schedules, budgets, risks, suppliers, and certification interfaces, and building a multidisciplinary engineering team. The role requires deep liquid bipropellant rocket engine experience, fluid and propulsion system analysis, component and plumbing design, hazardous operations leadership, test campaign experience, and stakeholder and proposal engagement.

Leads the structural engineering organization for an orbital launch vehicle, owning strategy, design authority, analysis, materials, manufacturing, testing, qualification, and delivery of primary structures including tanks, thrust structures, interstages, and fairings. Builds and mentors the structures, thermal, and mechanical engineering team while driving cross-functional integration, design-for-manufacture, structural verification, test correlation, and mass, robustness, cost, and schedule trade-offs.