Serve as a technical mentor across all ATD teams, including analysis, components, propulsion systems, engines, structures, and avionics
Collaborate closely with senior technical leaders, chief engineers, and cross-functional teams, including guidance, navigation, and control (GNC), structures, avionics, and systems engineering, to ensure seamless integration and performance optimization of ATD systems
Oversee the selection, design, evaluation, and testing of system components and subsystems (e.g., turbomachinery, valves, and injectors)
Conduct comprehensive analyses, simulations, and testing to validate and optimize the performance and reliability of ATD systems
Identify potential issues, manage technical risks, and develop mitigation plans to ensure successful system development and mission outcomes
Foster a culture of innovation, collaboration, and continuous improvement within the department
QUALIFICATIONS
Required
Bachelor's degree in Mechanical Engineering, Aerospace Engineering, or a related field
15+ years of experience in the design, development, and integration of propulsion and fluid systems for aerospace applications
Excellent leadership skills, with the ability to inspire and mentor a high-performing technical team
Proven track record of delivering complex systems projects from concept through flight qualification
Exceptional problem-solving and analytical skills, with keen attention to detail and a focus on delivering high-quality solutions
Strong communication and interpersonal skills, with the ability to collaborate
effectively with cross-functional teams and external stakeholders
Deep knowledge of mechanical design principles, fluid dynamics, combustion
processes, and thermal management for space applications
Passion for learning and teaching about advanced technology
Desired
Advanced degree in Mechanical Engineering, Aerospace Engineering, or a related field
Experience integrating, testing, and launching liquid-propellant launch vehicles
Proficiency in thermal analysis and optimization of propulsion systems to ensure reliable performance and safety
Proficiency in vehicle-level loads and environments, structural analysis, and
combined loads analysis
Familiarity with computational fluid dynamics (CFD), finite element analysis (FEA), and other simulation tools used in propulsion design and testing
Understanding of materials selection and manufacturing processes for launch vehicle and spacecraft components
Firefly offers outstanding benefits for our employees, including generous health, dental and vision plans with low plan deductibles, parental leave, relocation benefits, educational reimbursement, short term disability, and flexible PTO options.
To conform to U.S. Government space technology export regulations, including the International Traffic in Arms Regulations (ITAR) you must be a 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.
Firefly Aerospace, Inc. is an Equal Opportunity Employer; employment with Firefly is governed based on merit, competence and qualifications and will not be influenced in any manner by race, color, religion, gender, national origin/ethnicity, veteran status, disability status, age, sexual orientation, gender identity, marital status, mental or physical disability or any other legally protected status.
