Responsibilities:

• Support the development and verifying the implementation of the Fluids/Thermal Interface Control Documents (ICD) in MK1 lunar lander vehicle.
• Define tests and verifications activities for Mk1 lunar lander vehicle Fluids/Thermal ICD and own the verification Data package for the ICD
• Track thermal conductivity forMk1 vehicle major components to provide inputs for vehicle thermal analysis
• Review, scrub, and update MK1 vehicle Component Temperature List (CTL)
• Contribute to the development and documentation of Mk1 Fluids/Thermal vehicle requirements and verification data package
• Lead or contribute to the vehicle level risks focused on thermal and fluids integration areas

Qualifications

• B.S. in Aerospace Engineering, or Mechanical Engineering, or related technical subject area
• Deep technical knowledge in fluids and thermal subsystems in spacecrafts
• 2 years of experience with fluids/thermal aerospace engineering
• Proven track record in developing and managing ICDs
• Strong understanding of industry standards and regulations related to thermal and fluids systems in aerospace
• Knowledgeable of systems engineering practices, integration processes, and mission/safety critical systems
• Familiarity with relevant software tools (e.g. Ansys, Matlab, CFD software)
• Excellent verbal, written, and graphical communication skills
• Ability to work collaboratively in a fast paced, dynamic work environment
• Ability to earn trust, maintain positive and professional relationships, and contribute to a culture of inclusion

Desired (but not required):

• M.S. in Aerospace, Systems, Mechanical Engineering, or related technical subject area
• Experience in designing and integrating pressure and temperature interfaces in aerospace or any deep space lander systems
• 5 years of proven experience
• Experience with full spacecraft design life cycle