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Singularity Defense Corp. is seeking a Senior Solid Rocket Motor Engineer to lead propulsion design and structural analysis efforts across interceptor and munitions programs.
This senior IC role combines hands-on lab and production floor work with rigorous modeling, testing, and data validation to meet performance, safety, and regulatory requirements. The successful candidate will own ballistic performance prediction, mentor junior engineers, and contribute to program leadership in risk
We are seeking a Senior Solid Rocket Motor Engineer with expertise in propulsion system design and structural analysis. This is a senior individual contributor role with expectations for technical leadership, program ownership, and mentorship of junior engineers. The successful candidate will play a critical role in ensuring that propulsion components and assemblies meet rigorous performance, safety, reliability, and regulatory requirements while optimizing for weight, efficiency, and durability for interceptor, and munitions propulsion programs. This role demands hands‑on laboratory and production floor presence combined with the analytical rigor to own ballistic performance prediction and validation end-to-end.
Ballistic performance modeling for tactical motor configurations including boost, sustain, and dual‑thrust grain geometries common to surface‑to‑air, air‑to‑air, and ground‑launched systems. Develop and validate predictive models in SPP, CLWire, or equivalent tools, correlating strand burner and subscale motor data to full‑scale performance with confidence bounds. Characterize and model burn rate pressure exponent, temperature sensitivity, and erosive burning behavior under the wide operating temperature ranges (-65°F to +160°F) required of tactical systems. Lead ballistic anomaly investigations and author formal disposition packages. Participate in motor performance margin analysis and support trade studies during proposal and PDR/CDR phases.
Perform advanced structural and thermal analyses using Finite Element Analysis (FEA) tools (e.g., ANSYS, Abaqus, NASTRAN) to evaluate stress, strain, fatigue, vibration, buckling, and thermal loads under extreme operating conditions.
Design and execute comprehensive characterization programs covering mechanical properties (JANNAF strain invariant failure theory, uniaxial tensile, stress relaxation), burn rate (Crawford bomb, strand burner), and aging (HTPB hydrolysis, AP recrystallization, surveillance coupon programs). Analyze and interpret test data with statistical rigor, author technical reports, and present findings to program leadership and government customers. Serve as the technical point of contact for propellant‑related CDRLs and data submittals.
Provide day‑to‑day technical guidance to junior and mid‑level propellant engineers. Review and approve formulation and process documentation. Represent the team in integrated product team (IPT) settings and customer technical interchange meetings (TIMs). Contribute to IRAD initiatives, white papers, and proposal technical volumes. Help define and maintain the organization’s composite propellant technology roadmap. Assist with manufacturing and quality improvement processes. Assist with facility design and build out where expertise is relevant.
Serve as a senior resource for explosive safety compliance. Lead or support PHA, FMEA, and FTA activities for new propellant formulations and processing operations. Maintain awareness of ESD controls, friction/impact sensitivity protocols, and cook‑off behavior relevant to tactical motor environments. Participate in or lead mishap investigations and corrective action boards as required.
To conform to U.S. Government export regulations, applicant must be a (i) U.S. citizen or national, (ii) U.S. lawful, permanent resident (aka green card holder), (iii) Refugee under 8