The propulsion test engineer (PTE) will support senior engineers to oversee test design, conduct test operations, and configuration control in support of the Propulsion Test Branch at Marshall Space Flight Center. PTE will review test requirements, develop facility activation and operation procedures, and review test data. These tests will include launch vehicle systems, sub-systems, and component elements at various test facilities with the Propulsion Test Branch. PTE will provide test design documents and operational procedures for cryogenic and ambient propellant systems (hydrogen, oxygen), solid propellants, ancillary support systems (nitrogen, air, helium, hydraulics), and mechanical systems (thrust reaction, thrust measurement, structural loads).
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Job Type
Full-time
Career Level
Entry Level
Education Level
No Education Listed