We are looking for a Systems Engineer to lead the design, development, integration, testing, and qualification of monopropellant propulsion modules for CubeSats and small satellites. The role involves end-to-end development of propulsion subsystem hardware, including tank assemblies, structural components, propellant feed systems, valves, actuators, fill and drain systems, vent systems, thermal management systems, and associated mechanical and electrical interfaces.

The candidate will be responsible for system-level design, requirements development, component integration, interface management, verification, environmental qualification, and flight readiness of the propulsion module. The role requires strong systems engineering fundamentals, hands-on hardware development experience, and the ability to work across multidisciplinary engineering teams.

Responsibilities

- Lead the system-level design, development, and integration of monopropellant propulsion modules for CubeSats and small satellites.

- Develop propulsion subsystem architecture, functional requirements, system specifications, and component-level requirements.

- Work on propellant tank assemblies, including tank mounting, structural interfaces, fluid connections, sealing arrangements, and integration with the propulsion module.

- Design and integrate propellant feed systems, including tubing, fittings, manifolds, connectors, and associated fluid components.

- Work on integration of solenoid valves, latch valves, actuators, fill and drain valves, vent valves, and associated electromechanical interfaces.

- Work on thermal management systems,



including tank heaters, propellant line heaters, thermal sensors, insulation, and heater control interfaces.

- Coordinate with mechanical, electrical, electronics, thermal, manufacturing, and propulsion teams for hardware development and system integration.

- Plan and coordinate component-level and subsystem-level verification and validation activities.

- Lead propulsion module assembly, integration, inspection, functional checkout, and system-level testing.

- Develop qualification and acceptance test plans and support execution of environmental and functional testing, including vibration, shock, thermal vacuum, thermal cycling, leak testing, and pressure integrity testing, as applicable.

- Ensure compliance with applicable spacecraft mechanical, electrical, thermal, cleanliness, safety, and interface requirements.

- Prepare and maintain technical documentation, including test procedures, integration procedures, verification matrices, qualification reports, and system-level technical reports.

Requirements

- Solid understanding of mechanical systems engineering, fluid mechanics, thermodynamics, heat transfer, and aerospace engineering fundamentals.





- Experience in mechanical design and development of satellite subsystems, propulsion modules, or aerospace hardware.

- Knowledge of mechanical, electrical, fluidic, and thermal interface management.

- Understanding of pressure vessels, propellant tank assemblies, structural design, mounting interfaces, and mechanical packaging.

- Experience with fluid management systems, including valves, solenoids, actuators, tubing, fittings, manifolds, and sealing arrangements.

- Experience with thermal management systems, including line heaters, tank heaters, temperature sensors, insulation, and heater integration.

- Ability to develop system requirements, interface documents, verification matrices, test plans, and technical reports.

- Strong analytical, problem-solving, troubleshooting, communication, and multidisciplinary coordination skills.

Qualifications

- B.E./B.Tech or M.E./M.Tech in Aerospace Engineering, Mechanical Engineering, or any related discipline.

- 2+ years of experience in aerospace systems engineering, satellite subsystem development, propulsion systems, or mechanical and fluid systems design.

- Experience in the design, development, integration, and testing of aerospace hardware or pressure-containing systems.

Preferred Skills

- Experience in the development and qualification of CubeSat or small satellite propulsion systems.

- Previous experience with monopropellant propulsion modules, tank assemblies, and propellant feed systems.

- Familiarity with aerospace pressure vessels, propellant storage systems, and fluid-control components.

📌 Associate Scientist - System Engineering (Kanpur)
🏢 Dreamaerospace Technologies
📍 Kanpur