Senior Propulsion Engineer Solid Motors and Launch Assist Systems
Skills
About This Role
Company Description
Confidential.
Role Description
This is a full-time, on-site role located in the Abu Dhabi Emirate, United Arab Emirates, for a Senior Propulsion Engineer specializing in Solid Motors and Launch Assist Systems.
Responsibilities
include leading the development of solid rocket motor solutions for UAV assisted take-off applications.
This role covers the full propulsion product lifecycle, from concept design and detailed engineering through prototyping, testing, validation, and industrialization.
The ideal candidate has already worked on real propulsion hardware and knows how to move a design from development into repeatable, production-ready execution.
Key Responsibilities
- Lead the design and development of solid rocket motor systems for UAV-assisted take-off applications.
- Define system requirements, performance targets, interfaces, and integration needs with UAV platforms.
- Perform engineering analysis related to thrust, burn characteristics, chamber pressure, thermal behavior, structural integrity, and safety margins.
- Design propulsion-related components such as motor casing, nozzle, insulation, igniter interfaces, retention systems, and mounting hardware.
- Plan and manage prototype builds, including coordination with internal teams, suppliers, and manufacturing partners.
- Define and execute test campaigns, including ground testing, instrumentation setup, test procedures, data
- review, and post-test evaluation.
- Lead troubleshooting, root cause analysis, and design improvement activities following prototype and test results.
- Support industrialization by driving manufacturability, tooling concepts, process definition, inspection planning, and production readiness.
- Work closely with cross-functional teams including airframe, structures, manufacturing, quality, supply chain, and flight test.
- Prepare and maintain engineering documentation such as design reports, drawings, BOMs, test plans,
- qualification reports, and production documentation.
Qualifications
- Bachelor’s or Master’s degree in Aerospace Engineering, Mechanical Engineering, Propulsion Engineering, or a related field.
- Minimum 5 years of relevant experience in solid rocket motors, rocket propulsion, missile propulsion, or similar propulsion systems.
- Hands-on experience with CAD tools for propulsion component and assembly design, and CAE tools for
- engineering analysis and validation.
- Proven experience across design, prototyping, testing, and industrialization.
- Strong understanding of combustion, thermodynamics, structural design, thermal management, and propulsion system integration.
- Hands-on experience with prototype hardware development and propulsion testing.
- Experience preparing technical documentation for both development and production stages.
- Strong understanding of design for manufacturing, production transfer, and engineering support to
- manufacturing.
- Ability to work in a dynamic startup environment with a high level of ownership and accountability.
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