Independently plan, schedule and perform computations/analyses, prepare and make presentations, and document results in technical reports. Perform Thermal analyses in support of the design and design verification of solid rocket motors/propulsion systems. Analyze complex features of the work and apply principles and practices of thermal analysis, or devise new approaches in problem solutions. Review all results from assigned tasks and determine if outputs are complete, correct, integrated with project objectives, and adequately documented. Follow existing processes and procedures and recommend process improvements where appropriate.
Job duties:
BS degree in Mechanical, Electrical or Aerospace Engineering or related field from an ABET accredited institution is required. Minimum of 1 year experience using the Systems Improved Numerical Differencing Analyzer/Gaski (SINDA/G) code and a minimum of 3 years experience with PATRAN is desired. Familiarity with Ablation codes is desirable.
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