Create, review, and refine spacecraft component and subsystem mechanical designs in a modern CAD package (SolidWorks), managing small-to-medium assemblies
Develop clean-sheet mechanical and structural designs through detailed design, consistent with the risk posture, development velocity, and deployment schedules at Muon
Create quick concepts to drive early-phase discussions and inspire the team
Influence flight designs to ensure hardware is optimized for manufacturability, assembly, and testability
Make economically sound make vs. buy decisions, balancing the need to quickly demonstrate capability while understanding the path to scaled-up constellations
Analysis
Perform stress and dynamic analyses (hand calculations, simple FEM) to support and inform structural designs, including joint design, fastener sizing, and stiffness analyses
Collaborate with structural and thermal analysts to iterate designs for performance and manufacturability
Conduct trade studies to evaluate design alternatives and document recommendations
Support mass budget tracking and tolerance stack-up analyses for mechanical assemblies
Build & Integration
Create and maintain build procedures, assembly instructions, and work orders for mechanical hardware
Support and oversee technicians during assembly and integration of mechanical components and subsystems
Identify and resolve fit, form, and function issues during hardware builds
Drive designs toward producibility, considering prototype through production quantity needs
Conduct first article inspections (FAIs) and document non-conformances; participate in MRB as needed
Test & Verification
Design test fixtures and GSE to support development, qualification, and acceptance testing
Develop component and subsystem-level test plans and procedures for environmental testing (vibration, shock, TVAC)
Specify and integrate test instrumentation (accelerometers, strain gauges, thermocouples, etc.)
Execute and support environmental test campaigns; collect, reduce, and analyze test data
Document test results and correlate with analysis predictions; recommend design updates as needed
Documentation & Configuration Management
Create and maintain engineering drawings with proper GD&T, BOMs, and revision control
Author and maintain design documentation including trade studies, interface control documents (ICDs), and design rationale
Execute ECOs/DCOs and maintain configuration control through PLM systems
Document lessons learned from builds and tests to inform future designs
Collaboration & Coordination
Own delivery of mechanical items and subsystems, coordinating with analysts, avionics, program, thermal, optical, and RF engineers
Manage development of mechanical/structural architectures through detailed design in collaboration with cross-functional stakeholders
Coordinate with external vendors for part prototyping and development; review vendor deliverables for compliance with requirements
Present design status, trade studies, and test results at design reviews
Required Qualifications
5 years of experience designing, building, and testing flight hardware in the space industry (or similar: aerospace, autonomous vehicles, robotics, etc.)
B.S. or higher degree in Mechanical Engineering
Proficiency in CAD (SolidWorks preferred) for component and assembly design
Experience with engineering drawings, GD&T, BOMs, and ECO processes
Demonstrated experience executing structural or environmental tests and documenting results
Hands-on experience supporting hardware builds and integration activities
Strong documentation skills: ability to author clear build procedures, test plans, and technical reports
Excellent communication, presentation, and cross-functional coordination skills
A desire to change the way the world understands and reacts to climate and environmental data
Excited to work in a fast-paced environment with new opportunities each week
Nice-to-Have Skills
Experience with deployable structures (solar arrays, antennas, mechanisms) or SADA mechanisms
Experience running structural analyses for spacecraft (FEMAP, ANSYS, Nastran)
Experience with thermal management systems for spacecraft
Experience designing and executing qualification-level environmental tests (vibration, TVAC, shock)
Large assembly management in SolidWorks PDM; experience with PLM systems (Duro or similar)
Optomechanical instrument or payload design
Experience with composite materials and bonded assemblies
Experience managing external vendors for part prototyping and development
Software skills in Python, MATLAB, or similar for data analysis and automation
Familiarity with FAI processes, non-conformance reporting, and MRB activities
Google Workspace proficiency (Sheets, Slides, Docs); Slack
Salary
The salary range for this role is $144,000 - $177,000 plus a competitive equity grant and comprehensive benefits package. Final compensation will be based on skills, qualifications, experience, and geographic location as assessed during the interview process. ## Taking Care of Our Team
At Muon salary is only part of our total compensation package. In addition to salary, full-time employees receive equity compensation as well as benefits including medical, dental, and vision insurance, a 401k retirement plan, short & long term disability and life insurance. We also offer three weeks paid vacation for new employees, along with 12 paid holidays, unlimited sick time and paid parental leave. Our mission embraces the entire planet and we believe our team should too. Muon is dedicated to creating a diverse and dynamic company and workforce. We value diversity in the workplace, and that starts with our applicants. We encourage you to apply, even if you don't check all the boxes, and we look forward to reviewing your application! In addition, if you need a reasonable accommodation as part of your application for employment or interviews with us, please let us know. ## ITAR/EAR Requirements
This position requires access to export controlled information. To conform to U.S. Government export regulations applicable to that information, applicant must either be (A) a U.S. person, defined as a (i) U.S. citizen or national, (ii) U.S. lawful, permanent resident (green card holder), (iii) refugee under 8 U.S.C. § 1157, or (iv) asylee under 8 U.S.C. § 1158, (B) eligible to access the export controlled information without a required export authorization, or (C) eligible and reasonably likely to obtain the required export authorization from the applicable U.S. government agency. The Company may, for legitimate business reasons, decline to pursue any export licensing process.
