Designing mechanical components for space platforms such as satellites and orbital transfer vehicles by considering specified engineering requirements while prioritizing safety and efficiency,
Maintaining overall mass and balance constraints throughout the design process and conducting component- and structure-based lightweighting studies,
Designing mechanical systems including separation mechanisms, attitude control mechanisms, deployable power systems, hydraulic and pneumatic propulsion system equipment, and fuel distribution and storage equipment,
Performing mechanical design of enclosure housings required for electronic equipment and preparing manufacturing readiness and quality control documentation for designed parts,
Conducting vibration analyses for electronic equipment containing sensitive sensors and carrying out vibration isolation and damping studies,
Optimizing criteria such as fatigue and life calculations, material selection, assembly and integration ergonomics throughout system integration and design processes,
Having intermediate-level knowledge of aluminum, composites, and engineering plastics, and being able to design with manufacturability considerations in mind,
Managing design processes by carefully evaluating critical design points related to geometric dimensioning and tolerance stack-up analyses.
BASIC QUALIFICATIONS:
Pursuing or holding a bachelor’s degree in Mechanical Engineering, Aeronautical Engineering, Aerospace Engineering, or Mechatronics Engineering,
Experience with at least one 3D CAD software (preferably CATIA V5/V6 or similar),
Basic proficiency in computational engineering tools and applications (preferably MATLAB, Python, COMSOL, ABAQUS, LabVIEW, or PTC Creo).
PREFERRED SKILLS AND EXPERIENCE:
Ability to manage technical documentation processes such as work orders and operational instructions,
Knowledge of Bill of Materials (BOM) and Product Lifecycle Management (PLM),
Familiarity with optimization methods used in testing, analysis, and design processes.