Spacecraft C&DH Systems Lead Engineer

Recruiting; Canada; On-site; CAD 90,000 - 130,000; Full time

Job summary

Recruiting in Canada seeks an experienced Electrical/Aerospace Systems Engineer to translate mission-level requirements into C&D specifications and to produce System Requirements, ICDs, and description documents for spaceflight programs.

You will lead the design of on-board processors and data-bus interfaces (SpaceWire, MIL-1553, CAN, Ethernet), support RTOS/API discussions, IVV, and mentor junior engineers while ensuring data integrity and conformance to CCSDS/PUS standards.

Qualifications

• B.Sc. in Electrical Engineering, Aerospace or related field with 8 years of C&D engineering experience on LEO/MEO/GEO platforms.
• Deep knowledge of spacecraft data-bus standards: SpaceWire, MIL-1553, CAN-A, Ethernet, CCSDS packet telemetry/command and PUS services.
• Knowledge in processor, FPGA, firmware and embedded
• Strong understanding of aerospace system engineering fundamentals, space environment and orbit mechanics.
• Hands‑on individual who can support systems integration processes and capability to test systems and resolve problems.
• Experience with Confluence and JIRA.
• Demonstrated capability to efficiently work with little supervision.
• Ability to distill complex problems to fundamentals to solve with analysis, similarity, or creativity.
• Demonstrate excellent written and oral communication skills in English; knowledge of French will be considered an asset (Contact with clients outside Quebec and work on deliverables in English).

Responsibilities

• Translate mission-level requirements into C&D specifications.
• Produce System Requirements, ICDs, and Description documents.
• Perform requirement management and maintain bidirectional traceability throughout the project lifecycle.
• Collaborate with cyber-security to embed resilience and security by design, ECU.
• Lead detailed design of on-board processors, data-buses (SpaceWire, MIL-1553, CAN, Ethernet), memory subsystems, and I/O interfaces.
• Support software architecture: command sequencing, telemetry packetization, health-monitoring, services, fault-detection-isolation-recovery (FDIR).
• Support Satellite Reference Database development and validation
• Communicate technical status, risk assessments and trade-study results to senior management and/or customers or partners.
• Work with FSW teams to define RTOS, APIs, task scheduling, real-time OS configuration, services usage.
• Define uplink command formatting, downlink telemetry packet structures, and ground-segment data-handling interfaces (mission-control servers, data-archiving pipelines).
• Coordinate with TT&C/PDT engineering and Ground Segment ICDs to ensure end-to-end data integrity.
• Support B&P (Phase 0 & pre-phase A).
• Develop verification plans, test matrices, and validation procedures for unit, subsystem, and spacecraft level C&D tests.
• Execute functional tests, bus-protocol compliance, SIL and HIL campaigns.
• Manage anomaly investigations, root-cause analysis, and corrective-action implementation.
• Mentor, guide junior engineers and interns.
• Act as technical liaison with customers, partners and external vendors
• Act as Continuous Improvement stakeholder.
• Author and maintain C&D standards (bus protocols, data-format conventions, redundancy policies).
• Ensure all artefacts, analysis and documentations are version controlled in PLM environment.
• Support design reviews (SRR, PDR, CDR, MRR/TRR…etc.).
• Support Technology Road-Mapping & Innovation
• Support launch-pre-launch and early-orbit checkout, validate satellite functions, HK and nominal operation
• Support and analyse on-orbit telemetry, update filter parameters as needed.
• Support SOOH development and associated operator trainings

Skills

SpaceWire

MIL-1553

CAN-A

Ethernet

CCSDS

PUS services

Confluence

JIRA

Education

B.Sc. in Electrical Engineering, Aerospace or related field

Tools

PLM

Job description

Recruiting in Canada seeks an experienced Electrical/Aerospace Systems Engineer to translate mission-level requirements into C&D specifications and to produce System Requirements, ICDs, and description documents for spaceflight programs.

You will lead the design of on-board processors and data-bus interfaces (SpaceWire, MIL-1553, CAN, Ethernet), support RTOS/API discussions, IVV, and mentor junior engineers while ensuring data integrity and conformance to CCSDS/PUS standards.