Job Description

Description

Description

The Department of Aerospace Engineering in the College of Engineering at the University of Michigan in Ann Arbor is seeking a Research Investigator. This position is a one year term-limited appointment with possibility of extension contingent upon funding availability.

Chief engineer for propulsion (SPAR)

• Overseeing the technical efforts of a national team of universities and small businesses developing advanced propulsion concepts for the SPAR institute
• Coordinating and executing on several systems-level integrated tests for the propulsion team. Key subsystems to be integrated include flow system, power processing, and engine head
• Overseeing efforts at University of Michigan to implement upgraded hydrazine-compatible test facilities for propulsion testing
• Supporting the maintenance and use of the alternative gas test facility capable of testing high-power (> 100 kW) thruster concepts

Technical lead (DARPA)

• Serving as a liaison and test lead for projects with commercial partners (5 universities and 5 small businesses)
• Supporting ongoing test activities on Hall thrusters, rotating magnetic field thrusters, advanced hollow cathodes, and magnetic nozzles
• Leading development and maintenance of diagnostics
• Assisting in maintaining a culture of lab safety
• Assisting in the mentorship of doctoral students in the group
• Assisting in the writing and preparation of proposals for sponsored grant research

Additional Information

This position is subject to final administrative approval. This position is a one year term-limited appointment.

Background Screening

The University of Michigan conducts background checks on all job candidates upon acceptance of a contingent offer and may use a third party administrator to conduct background checks. Background checks are performed in compliance with the Fair Credit Reporting Act.

Qualifications

Required Qualifications

• PhD in aerospace or related engineering discipline
• Experience with cryogenic pumping vacuum systems
• Experience with Hall thruster testing at power levels above 5 kW
• Experience with the implementation and analysis of standard electric thruster diagnostic suites
• Experience with hollow cathode development and power processing development
• Experience in leadership of technical teams
• Eligibility for USG Secret clearance

Application Instructions

To apply, please upload a cover letter, CV, and list of professional references to the Interfolio application link

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