Position Description

This position is for a Propellant Transfer System (PTS) electrical engineer that will be responsible for flight electrical design and EGSE for the PTS. This work includes developing electrical designs, block diagrams, EICDs, wire lists, harness drawings, work instructions and procedures, generating schematics, preparing test readiness reviews, conducting the testing and writing test reports. Work also includes assembling hardware and maintaining the equipment including electrical test equipment. The electrical engineer will report to the PTS lead, attend regular PTS meetings to stay current on developments outside the normal activities, and provide electrical support to the PTS team. The work will be conducted at NASA Goddard Space Flight Center in Greenbelt, MD, and some travel may be required.

Position Requirements

1. BS in aerospace or electrical engineering or equivalent experience is required.
2. 5 years of related experience
3. 2 years of experience with harness design
4. Ability to conduct electrical test

A preferred candidate would have 6+ year experience in aerospace or electrical engineering with focus on propulsion systems. The candidate would also have experience with launch vehicle or spacecraft propulsion flight hardware and experience with leading an electrical test campaign.