Senior/Principal Propulsion Engineer
Listed on 2025-12-02
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Engineering
Aerospace / Aviation / Avionics, Mechanical Engineer, Systems Engineer
Overview
Rocket Lab is an end-to-end space company delivering responsive launch services, complete spacecraft design and manufacturing, payloads, satellite components, and more – all with the goal of opening access space. The Space Systems business designs and builds satellites, payloads, and components, including spacecraft selected to support NASA missions to the Moon and Mars and components used on the James Webb Space Telescope.
Neutron is a medium-lift launch vehicle capable of delivering the mega constellations of tomorrow, high-assurance payloads, and human spaceflight. As a highly reusable launch platform, Neutron will deliver a cost-effective and reliable launch solution leveraging Rocket Lab’s proven execution history with the Electron program. This is an opportunity to join a high-performing team and contribute to a clean-sheet development of a reusable liquid launch vehicle.
RoleSENIOR / PRINCIPAL PROPULSION ENGINEER
As Senior/Principal Propulsion Engineer, you will play a critical role in the development, testing, and operation of the Archimedes Engine family, a cornerstone of the Neutron rocket program. You will take ownership of subsystems and engine operation, driving design, analysis, testing, and operational readiness. You will execute testing campaigns, analyze data, improve existing evaluation capability and refine designs for reliability and vehicle operations.
This role demands technical expertise, strong autonomy, and the ability to align teams and projects to achieve program goals. Principal Engineers will additionally drive value to teams outside their group, influencing cross-functional efforts and contributing to the broader success of the Neutron program.
- Design, analyze, test, fly, and refly next generation propulsion hardware ensuring operational readiness and flight success.
- Develop and execute test plans, including qualification and acceptance testing, and conduct post-test data reviews to refine designs and processes.
- Collaborate across engineering disciplines to optimize engine performance, reliability, and manufacturability.
- Generate high-level plans and prioritize tasks across teams, resolving competing priorities and ensuring alignment with program goals.
- Mentor and guide engineers, fostering technical growth and collaboration.
- Work with manufacturing, testing and vehicle operation teams to support engine needs, operation, and resolve issues at each part of the engine lifecycle.
(This position can be hired as a Senior Propulsion Engineer I, II or Principal Propulsion Engineer)
QualificationsYou’ll bring these qualifications as a Senior Propulsion Engineer I
- Bachelor’s degree in mechanical engineering, aerospace engineering, or related field.
- 5+ years of experience in rocket engine development, testing, or operations.
- Strong technical understanding of fluid dynamics, thermodynamics, cryogenic systems, and rocket engine architecture.
- Familiarity with engine P&IDs, fluid system routing, and hotfire data reviews.
You’ll bring these qualifications as a Senior Propulsion Engineer II
- Bachelor’s degree in mechanical engineering, aerospace engineering, or related field.
- 8+ years of experience in rocket engine development, testing, or operations.
- Strong technical understanding of fluid dynamics, thermodynamics, cryogenic systems, and rocket engine architecture.
- Familiarity with engine P&IDs, fluid system routing, and hotfire data reviews.
You’ll bring these qualifications as a Principal Propulsion Engineer
- Bachelor’s degree in mechanical engineering, aerospace engineering, or related field.
- 12+ years of experience in rocket engine development, testing, or operations.
- Strong technical understanding of fluid dynamics, thermodynamics, cryogenic systems, and rocket engine architecture.
- Familiarity with engine P&IDs, fluid system routing, and hotfire data reviews.
Nice-to-have
- Advanced degree in a fluid mechanics-heavy field.
- Experience with ox-rich staged combustion systems and methyl/LOX propellants.
- Background in failure analysis, combustion dynamics, turbopump mechanics, and hydraulics.
- Familiarity with reusable rocket engine systems and test/launch facility operations.
- Expe…
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