Sr. Structural Analyst - Aerospace Launch Vehicle

Mavensoft Technologies, LLC; Kent (WA); On-site; USD 110,000 - 160,000; Full time

Job summary

Mavensoft Technologies, LLC is seeking a Sr. Structural Analyst for an Aerospace Launch Vehicle project in Kent, WA. This onsite role spans the full hardware lifecycle from concept through launch, focusing on strength analysis of primary and secondary structures.

Responsibilities include hand calculations, FEM, and collaborating with manufacturing to ensure successful hardware integration. Requires 6+ years in aerospace structures and proficiency with CAD/FEA tools.

Qualifications

• Minimum of a B.S. degree in engineering with 6+ years of aerospace structures experience.
• Experience on aircraft, spacecraft, or launch vehicle structures and load paths.
• Proficiency in industry standard analysis codes and CAD/FEA tools.

Responsibilities

• Own hardware lifecycle from requirements to integration.
• Analyze and test primary/secondary metallic and composite structures.
• Perform hand calc and FEM analyses for margins of safety.
• Document stress analyses to support release of drawings.
• Lead design concepts, trade studies, and risk/ performance evaluations.
• Build system and detail models for structural design.
• Plan and execute structural tests and report results.
• Present technical content to internal/external customers.
• Collaborate across design, manufacturing, and mission teams.

Skills

FEA/Structural analysis

Ansys/Nastran/OptiStruct/HyperMesh

CAD (Creo/Windchill)

Composite/metallic design

Hand calculations

FEM analysis

Bolted joint design

Documentation & reporting

Strong communication

Education

B.S. in engineering

Tools

Ansys

Nastran

OptiStruct

HyperMesh

Creo/Windchill

Job description

Sr. Structural Analyst -Aerospace Launch Vehicle

• Kent, WA

Job title: Sr. Structural Analyst -Aerospace Launch Vehicle

Work location: Onsite in Kent, WA

Duration: 6 months

Terms: W2 Contract

Position Summary

• This role supports the development of a heavy-lift orbital launch vehicle capable of routinely carrying people and payloads to low-Earth orbit, geostationary transfer orbit, cislunar, and beyond.
• This position will be directly involved in the design of the next progression of hardware.
• As part of a small, hardworking team of engineers, you will be responsible for strength analysis of primary and secondary structures.
• In this role, you will take ownership of designs from concept through launch, perform initial sizing, analysis, development, testing, and qualification of structural subsystems, and work directly with our manufacturing teams to ensure successful hardware integration.

Responsibilities

• Take ownership of the full lifecycle of hardware from requirements definition through concept development, design, analysis, testing, qualification, and integration.
• Analyze, develop, and test primary and secondary metallic and composite unpressurized structures.
• Complete hand calc and FEM analyses to report margins of safety for primary and secondary aerospace structures.
• Documentation of stress analysis to support release of engineering drawings and documents.
• Perform research, develop concepts, and run trade studies providing technical guidance (risk vs. cost vs. performance)
• Build system and detail level models supporting structural design.
• Take ownership of structural test planning, execution, data reduction, analysis, and authoring of test reports.
• Prepare technical content and present to internal and external customers.
• Collaborate with internal and external teams throughout design, manufacturing, and mission integration.

Required Qualifications

• Minimum of a B.S. degree in engineering and 6+ years of experience with aircraft, spacecraft, or launch vehicle structures.
• Must be a U.S. citizen or national, U.S. permanent resident (current Green Card holder), or lawfully admitted into the U.S. as a refugee or granted asylum.
• Experience with recently developed aircraft or launch vehicles in one or more of the following areas: Vehicle load path distribution, and first order strength assessment and sizing. Skin-stringer, orthogrid, isogrid, and composite sandwich panel design.
• Experience working in a multi-functional organization to develop designs and produce world-class engineered products.
• Strong understanding of composite and metallic design fundamentals.
• Demonstrated expertise with any industry standard analysis codes: Ansys, Nastran, OptiStruct, HyperMesh.
• Experience in bolted joint design and analysis.
• Structural design experience using CAD (Creo/Windchill preferred), hand calculations, and FEA tools.
• Ability to take ownership of the hardware lifecycle from requirements definition through concept development, design, analysis, testing, qualification, and integration onto a launch vehicle.
• Strong written and verbal communication skills.
• Collaborative attitude and effective interpersonal skills.
• Self-motivated with a strong desire to learn, take ownership, and drive projects to completion.

Preferred Qualifications

• Experience with rapid development techniques for hardware.
• Experience with fabrication using automated fiber placement (AFP) and tape laying (ATL).
• Experience or expertise in fabrication of large-scale out-of-autoclave composite structures.
• Demonstrated experience developing manufacturing processes for transition to production.
• Knowledge of systems engineering practices, fabrication and integration processes, and quality control.
• Experience with Optimization and Design of Experiments (DOE) methods as applied to design, analysis, and testing.

Authorized US Worker

US Citizens and those authorized to work in the US are encouraged to apply. We are unable to sponsor at this time.