p>Qualifications: • Bachelors degree in Mechanical or Aerospace Engineering, or a related field • A minimum of 6 years of experience in analysis and design • Expert knowledge of finite element analysis, structural dynamics, thermal loading, and problem solving skills • Strong technical knowledge of cryogenic systems • Experience in specifying launch or space vehicle testing requirements of low/high cycle fatigue, fracture, creep, shock, and vibration response tests • Experience managing requirements, verifications, and certification documents • Proficient in simulation tools (such as ANSYS or NASTRAN) and CAD software (such as CREO, NX, Catia) • Experience with industry and regulatory requirements such as NASA-STD-5020, ANSI/AIAA S-080A-2018, JSC 65829 • Ability to work effectively in a fast-paced, multidisciplinary team environment • Ability to work with early career engineers and mentor with best practices for low fidelity structural analysis and review of these packages • Excellent written and verbal communication skills, including the ability to communicate technical concepts to non-technical audiences.
Desired:
• Masters or PhD in Mechanical/Aerospace Engineering or related field • Successfully designed, analyzed, qualified, and launched space vehicle hardware (including valves, turbomachinery, and pressure vessels) • Knowledge and familiarity with fatigue and fracture mechanics • Experience in executing launch or space vehicle testing, including low/high cycle fatigue, fracture, creep, shock, and vibration response tests • Experience in resolving anomalies, conducting investigations, presenting/dispositioning high value mission critical engineering significant non-conformances • Experience chairing at decision making meetings.