Projects may include supporting areas such as mechanical design, CAD modeling, thruster design and system integration technology.
Tasks will likely involve assisting with the development of engineering designs that are used on liquid rocket engine applications, including the successful planning, design, development and qualification of mechanical hardware. This may include conceptual design support, part selection research and computer aided design (CAD) as well as data collection, entry level analysis and hardware tracking. Interns will utilize computer aided design (CAD) and product lifecycle management software tools such as Windchill.
Candidate must be currently enrolled in an undergraduate or graduate degree program in Mechanical Engineering or Aerospace Engineering (or similar major) and returning to school upon completion of the assignment.
Preferred Qualifications
3.2 GPA or above
Junior standing or above
Solid academic track record of accomplishment
Working knowledge of Microsoft Software applications (Excel, Word, PowerPoint)
Excellent communication and problem-solving skills
Leadership & teamwork skills
Coursework in engineering design, structural analysis, computer aided design
Experience with development hardware, mechanical assembly and/or test
Working knowledge of CAD software tools such as CREO or Solidworks
Experience with Windchill PLM
