
Description
Description
This role involves evaluating and estimating launch vehicle flight and mechanical ground support equipment loads; assessing mechanical design of vehicle components, subsystems, and handling equipment; evaluating load and mechanical stress analysis; overseeing proof load and flight acceptance load testing; processing, analyzing, and visualizing coupled loads and control bending modes analysis; reviewing requirements and tailoring performed by launch vehicle contractors; supporting hardware acceptance and pedigree reviews; producing analysis reports of test and post-flight data; and presenting analysis and predictions to a technical audience in formal and informal contexts. This role works in coordination with a multi-disciplinary team performing independent validation and verification (IV&V) on rocket launch vehicles to support launch programs on an aggressive schedule. This role may require significant travel (~25%) to support testing and reviews.
Qualifications
Requirements:
- A BS degree in Mechanical Engineering, Aerospace Engineering, Engineering Physics, or a related discipline and a minimum of five (5) years of applicable industry OR three (3) years and a MS degree from an ABET-accredited school
- Experience with strain gage application and data evaluation using Matlab, NumPy/SciPy
- Strong understanding of basic theory and application of principles of mechanical design and structural analysis including pressurized systems, modal analysis, discrete Fourier transform (DFT) frequency domain methods
- Solid understanding of structural mechanics including non-linear stress/strain curves, fatigue and fracture analysis, corrosion mechanisms, thermal stress effects
- Strong Experience with structural analysis (both closed form and using finite element tools) with static and dynamic loading
- A basic understanding of multiple engineering disciplines including aerofluids, dynamics, propulsion, GN&C, avionics and willingness to learn on the job
- Practical experience working in an engineering environment including standard processes for evaluating engineering change proposals, reviewing technical analyses, supporting Design Reviews (SRR/PDR/CDR)
- Strong work ethic and self-motivated to learn tools and techniques in other technical areas
- The ability to obtain a DoD SECRET or TOP SECRET clearance is mandatory (must be a US Citizen, no felony convictions or pending criminal indictments, et cetera)
Desired:
- Knowledge of applicable military and industry standards including MIL-STD-1540/SMC-S-016, AIAA S-110, AIAA S-114, SMC-S-013, AS9100,
- Experience with doing space launch vehicle component, subsystem, and payload structural and modal testing including evaluating test setup, ‘notching', debugging test issues, et cetera
- Experience with anomaly/failure analysis including the use of fault trees, failure modes and effects analysis, statistical failure estimation, et cetera
- Experience with component development, reliability analysis, statistics, and aging surveillance testing
- Ability to develop, document, and improve robust data processing and analysis tools using Python, Matlab, C, Fortran, or other languages
Target salary range: $80,001 - $120,000. The estimate displayed represents the typical salary range for this position based on experience and other factors.
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