Mechanical Design Engineer

AST SpaceMobile is developing a space-based cellular broadband network accessible by standard smartphones. The Mechanical Design Engineer supports satellite mechanical subsystem and payload development through structural architecture, design, analysis, interface management, documentation, assembly, and test support.

Responsibilities:

• Perform mechanical design and computer-aided modeling of space hardware, including final detailed design definition of parts and assemblies and management of mechanical interfaces between subsystems
• Conduct structural, mechanical system, and satellite payload equipment layout studies to determine optimal system architecture in terms of simplicity, performance, mass, and cost
• Develop and maintain mechanical and structural design documentation at system and equipment level: mechanical analysis reports, interface control drawings, tooling and fixturing, and manufacturing documentation
• Support creation of developmental and qualification test procedures (vibration, shock, TVAC, assembly)
• Prepare and present the information required to conduct thorough design and readiness reviews with management and peers
• Coordinate with manufacturing and production to ensure successful transfer of information and that efficient processes are understood and documented
• Evaluate and champion new technologies and methods

Requirements:

• Bachelor's degree in mechanical engineering, aerospace engineering, or a related technical field
• A minimum of 12 years of hands-on experience in mechanical design, integration, and testing of spacecraft and spacecraft components
• Innovative and creative approach to problem solving, with a willingness to challenge the status quo
• Demonstrated ability to work in a multidisciplinary team with other engineers
• Ability to lead a small team while also carrying assignments autonomously
• Flexibility and adaptability in a fast-paced, dynamic environment
• Excellent English written and verbal communication skills
• CATIA, SolidWorks, or CREO
• an advanced degree is preferred
• Strong technical skill in design of satellite assemblies for launch and on-orbit environments, as well as design for manufacturability
• Experience using standard analytical tools and classical structural analysis methods to support sizing and trade studies
• Knowledge of, or experience with, launch vehicle integration
• Experience operating in a Windchill PLM environment
• Advanced degree in mechanical or aerospace engineering
• Siemens NX preferred