Senior Dynamics Analysis Engineer
True Anomaly
$135,000 - $200,000 / year
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Description
Space is a warfighting domain. True Anomaly seeks those with the talent and ambition to build the technology that secures it.
OUR MISSION
True Anomaly delivers decisive capabilities for space superiority. We build autonomous spacecraft, advanced payloads, mission software, and space-based interceptors — enabling the U.S. and its Allies to secure the space environment and counter threats from the ultimate high ground.
OUR VALUES
- Be the offset. We create asymmetric advantages with creativity and ingenuity.
- What would it take? We challenge assumptions to deliver ambitious results.
- It’s the people. Our team is our competitive advantage and we are better together.
BENEFITS & PERKS*
- Best-in-class healthcare: 100% company-paid medical, dental, and vision coverage for you and your dependents, with HSA/HRA options
- Generous time off: Flexible Time Off (FTO) for exempt employees, accrued PTO of up to 25 days for non-exempt employees, plus 12 paid holidays; Parental Leave; Sick Leave
- Fuel for your day: Daily catered lunch and unlimited snacks for in-office employees
- And more: 401(k) retirement plan, fitness reimbursement, and Dog Fridays
- Equity participation: Equity is included as part of our total compensation package, giving you an opportunity to share in the company’s success.
*Do not apply to fixed term and temporary roles
YOUR MISSION
True Anomaly is seeking a skilled and experienced Senior Dynamics Analysis Engineer to join our Mechanisms team, reporting to the Mechanisms Engineering Manager. In this role, you will be the technical authority for structural dynamics analysis across our spacecraft mechanism and actuation systems — from launch load environments through on-orbit disturbance and pointing stability. You will develop and own finite element models, execute modal, random vibration, shock, and frequency response analyses, and translate results into actionable design guidance for the mechanisms and broader spacecraft engineering teams. You bring deep analytical expertise, a hands-on approach to test correlation, and the ability to work fluidly across mechanical, GNC, and systems engineering disciplines to ensure our hardware performs reliably from the pad to orbit.
RESPONSIBILITIES
- Develop, maintain, and validate finite element models (FEMs) for spacecraft mechanism and actuation system components and assemblies
- Perform structural dynamics analyses including modal analysis, frequency response, random vibration, shock response, and quasi-static load analysis across launch and on-orbit environments
- Develop and maintain mechanism-level disturbance models, including jitter and vibration disturbance budgets, and assess impacts on pointing stability and spacecraft performance
- Collaborate with the GNC team to characterize and mitigate dynamic disturbances from actuation systems affecting attitude control and pointing accuracy
- Define and support dynamic test campaigns including modal surveys, sine sweep, random vibration, and shock testing; correlate FEM predictions with test data
- Translate analysis results into clear design recommendations and margin assessments, driving design changes where needed
- Support mechanism trade studies, design reviews, and qualification activities with dynamics analysis inputs
- Develop and maintain analysis documentation including model descriptions, analysis reports, and test correlation records
- Mentor junior engineers and contribute to the continuous improvement of structural dynamics processes and tools
QUALIFICATIONS
- Bachelor's degree in Mechanical Engineering, Aerospace Engineering, or related field (Master's preferred)
- 5+ years of professional experience in structural dynamics analysis for aerospace, defense, or high-reliability applications
- Demonstrated proficiency with FEA tools for structural dynamics (NASTRAN, ANSYS, or equivalent)
- Experience with modal analysis, random vibration, shock response spectrum (SRS), and frequency response analysis
- Familiarity with launch vehicle interface requirements and coupled loads analysis processes
- Experience supporting or interpreting dynamic environmental test campaigns and correlating results with FEM predictions
- Ability to work cross-functionally with mechanical design, GNC, and systems engineering teams
- Excellent written and verbal communication skills
PREFERRED SKILLS AND EXPERIENCE
- Experience with spacecraft mechanism or actuation system dynamics, including jitter analysis and disturbance budgeting for precision pointing applications
- Familiarity with GNC interface requirements and the impact of structural dynamics on attitude control performance
- Experience with coupled loads analysis (CLA) and launch vehicle ICD compliance
- Knowledge of fatigue and fracture mechanics analysis methods
- Familiarity with test-analysis correlation methods and model updating techniques
- Experience with Python, MATLAB, or similar tools for post-processing and automating analysis workflows
- Experience working in a fast-paced, startup environment or a similarly dynamic setting
COMPENSATION
- Base Salary: $135,000 - $200,000
- Equity + Benefits including Health, Dental, Vision, HRA/HSA options, PTO and paid holidays, 401K, Parental Leave
Your actual level and base salary will be determined on a case-by-case basis and may vary based on the following considerations: job-related knowledge and skills, education, location, and experience.
ADDITIONAL REQUIREMENTS
- Ability to maintain or obtain TS//SCI clearance
- Work Location: Successful candidates will be located near our Centennial, CO or Long Beach, CA locations. While we observe a hybrid work environment, some work must be done on site.
- Work Enviornment: the work environment; temperature, noise level, inside or outside, or other factors that will affect the person's working conditions while performing the job.
- Physical Demands: the physical demands of the job, including bending, sitting, lifting and driving.
This position will be open until it is successfully filled. To submit your application, please follow the directions below. #LI-Onsite
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.
True Anomaly is committed to equal employment opportunity on any basis protected by applicable state and federal laws. If you have a disability or additional need that requires accommodation, please do not hesitate to let us know.
To protect candidates and our company from application fraud and impersonation, we use third-party tools to verify applicant identity and detect fraudulent applications. Learn more in our Privacy Notice.
Benefits
- Best-in-class healthcare: 100% company-paid medical, dental, and vision coverage for you and your dependents, with HSA/HRA options
- Generous time off: Flexible Time Off (FTO) for exempt employees, accrued PTO of up to 25 days for non-exempt employees, plus 12 paid holidays; Parental Leave; Sick Leave
- Fuel for your day: Daily catered lunch and unlimited snacks for in-office employees
- And more: 401(k) retirement plan, fitness reimbursement, and Dog Fridays
- Equity participation: Equity is included as part of our total compensation package, giving you an opportunity to share in the company’s success.
- Develop, maintain, and validate finite element models (FEMs) for spacecraft mechanism and actuation system components and assemblies
- Perform structural dynamics analyses including modal analysis, frequency response, random vibration, shock response, and quasi-static load analysis across launch and on-orbit environments
- Develop and maintain mechanism-level disturbance models, including jitter and vibration disturbance budgets, and assess impacts on pointing stability and spacecraft performance
- Collaborate with the GNC team to characterize and mitigate dynamic disturbances from actuation systems affecting attitude control and pointing accuracy
- Define and support dynamic test campaigns including modal surveys, sine sweep, random vibration, and shock testing; correlate FEM predictions with test data
- Translate analysis results into clear design recommendations and margin assessments, driving design changes where needed
- Support mechanism trade studies, design reviews, and qualification activities with dynamics analysis inputs
- Develop and maintain analysis documentation including model descriptions, analysis reports, and test correlation records
- Mentor junior engineers and contribute to the continuous improvement of structural dynamics processes and tools
- Bachelor's degree in Mechanical Engineering, Aerospace Engineering, or related field (Master's preferred)
- 5+ years of professional experience in structural dynamics analysis for aerospace, defense, or high-reliability applications
- Demonstrated proficiency with FEA tools for structural dynamics (NASTRAN, ANSYS, or equivalent)
- Experience with modal analysis, random vibration, shock response spectrum (SRS), and frequency response analysis
- Familiarity with launch vehicle interface requirements and coupled loads analysis processes
- Experience supporting or interpreting dynamic environmental test campaigns and correlating results with FEM predictions
- Ability to work cross-functionally with mechanical design, GNC, and systems engineering teams
- Excellent written and verbal communication skills
- Experience with spacecraft mechanism or actuation system dynamics, including jitter analysis and disturbance budgeting for precision pointing applications
- Familiarity with GNC interface requirements and the impact of structural dynamics on attitude control performance
- Experience with coupled loads analysis (CLA) and launch vehicle ICD compliance
- Knowledge of fatigue and fracture mechanics analysis methods
- Familiarity with test-analysis correlation methods and model updating techniques
- Experience with Python, MATLAB, or similar tools for post-processing and automating analysis workflows
- Experience working in a fast-paced, startup environment or a similarly dynamic setting
- Base Salary: $135,000 - $200,000
- Equity + Benefits including Health, Dental, Vision, HRA/HSA options, PTO and paid holidays, 401K, Parental Leave
- Ability to maintain or obtain TS//SCI clearance
- Work Location : Successful candidates will be located near our Centennial, CO or Long Beach, CA locations. While we observe a hybrid work environment, some work must be done on site.
- Work Enviornment: the work environment; temperature, noise level, inside or outside, or other factors that will affect the person's working conditions while performing the job.
- Physical Demands: the physical demands of the job, including bending, sitting, lifting and driving.
About this role
True Anomaly is building autonomous spacecraft and space-based systems for U.S. defense, and this role puts you at the center of ensuring those systems perform reliably from launch through orbit. As Senior Dynamics Analysis Engineer on the Mechanisms team, you'll own structural dynamics analysis for spacecraft mechanisms and actuation systems—developing and validating finite element models, running modal and vibration analyses, and translating results into design guidance that keeps hardware performing under extreme conditions. You'll work across mechanical, guidance/navigation/control, and systems engineering teams to characterize disturbances, support test campaigns, and drive design decisions that matter.
The position demands 5+ years of aerospace or defense dynamics experience and strong proficiency with FEA tools like NASTRAN or ANSYS. You'll need hands-on familiarity with modal analysis, random vibration, shock response, and test correlation—and ideally experience with spacecraft mechanisms, jitter analysis, or coupled loads processes. This is a technical authority role, so you should be comfortable mentoring junior engineers and owning analysis documentation alongside the day-to-day engineering work.
This is a temporary, in-office position in the Denver area, with a salary range of $135,000–$200,000 plus equity, comprehensive healthcare, flexible time off, and catered lunches. The role suits someone with deep structural dynamics expertise who thrives in a fast-paced, mission-driven environment and wants hands-on involvement in space defense technology.
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$135,000 to $200,000 per year
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