venusaero - Venus Aerospace - Principal Propulsion Engineer (Liquid Rocket Engine Assembly RE)

• 10+ years of aerospace vehicle and engine systems engineering/design experience • Bachelor’s degree in aerospace or mechanical engineering • Systems engineering and operational experience • Experience working on multidisciplinary project teams • Knowledge of standard aerospace materials used in designs of propulsion systems for high mechanical and thermal loads • Knowledge of aerospace fluid systems component and fluid connections specifications • 5+ years of CAD experience, particularly working with large assemblies • Experience in some of the design and analysis tools such as NX / SolidWorks, ANSYS mechanical, CFX / StarCCM+, Matlab / Python, GFSSP, Microsoft Visio • Strong communication skills to effectively work in a hybrid in-person/remote work environment • ## What Will Set You Apart • Master’s, PhD degree in aerospace or mechanical engineering • Project management/leadership • Familiarity with Agile methods • Strong background in systems engineering for engine or PPMS systems • Engine and/or engine component testing • Familiarity with standards such as SMC-S-016, NASA STD-5012, AIAA S-080A-2018 • Experience developing and standardizing processes for design, analysis, and testing • Responsible engineer experience in hotfire testing of liquid rocket engine assemblies, especially those that have gone wrong. • This position involves access to technology that is subject to U.S. export controls. Any job offer made will be contingent upon the applicant’s capacity to serve in compliance with U.S. export controls. To conform to U.S. Government space technology export regulations, including the International Traffic in Arms Regulations (ITAR) you must be able to meet ITAR requirements (U.S. citizen, lawful permanent resident of the U.S., protected individual as defined by 8 U.S.C. 1324b(a)(3), or eligible to obtain the required authorizations from the U.S. Department of State). You can learn more about ITAR here.