Liquid Rocket Research Engineer

DUTIES AND RESPONSIBILITIES: Join an established team of engineers and program managers in the Integrated Rocket Systems Branch of the Air Force Research Laboratory, Rocket Propulsion Division (AFRL/RQR) performing research, and development on various missile, rocket systems, space propulsion, and launch vehicle technologies to enhance the nation’s Missile and Space capability. Responsibilities would span from aiding internal research and external technology development efforts, facilitating flight-testing activities on a high tempo development program, evaluating contractor progress, and tracking progress of external contracts. These activities include overseeing and supporting the government project managers on design, fabrication, and testing of flight test articles, test campaigns, reviews, and program planning. Furthermore, the Research Engineer would perform design/evaluation of various propulsion concepts, developing test plans, schedules, and procedures, visiting contractor and test facilities to ensure program goals are met within budget and schedule. The engineer will focus heavily on applied technology and demonstration efforts with a heavy emphasis on technology transition. The selected individual’s activities will often span various disciplines such as missile design, liquid rocket engines, solid rocket motors, integrated vehicle systems, flight system integration, and operational evaluations. The group has extensive collaborations with other portions of the Air Force and Space Force, as well as other government agencies including NASA, and industry, and the candidate will be working closely with many other organizations. Travel will be required.

REQUISITE SKILLS: A self-motivated drive of increasing one’s expertise and familiarity within a new technical discipline or technical area. An experienced hard-working, go-getter passionate about rockets. The successful candidate needs to be independent, driven, motivated. They need to be able to identify what needs accomplished and pursue objectives with minimal guidance. An understanding of thermodynamics, fluid mechanics, and heat transfer. A systems thinking approach to problem solving. Familiarity with rocket propulsion desirable. Familiarity with testing of complex systems desirable. The candidate shall have a good command of Microsoft Office software (Word, Excel, and PowerPoint). A good knowledge of the English language is required. The candidate shall be able to operate in a team environment, and shall have excellent interpersonal, reporting and communication skills (written and verbal).

QUALIFICATIONS: Candidates must have earned a B.S. degree or higher in Aerospace, Mechanical, or Systems Engineering or a similar discipline. The candidate must be a US citizen and be able to obtain a US security clearance.