General Atomics Aeronautical Systems ยท 7 hours ago
Propulsion Engineer
General Atomics Aeronautical Systems, Inc. (GA-ASI) is a world leader in remotely piloted aircraft and tactical reconnaissance radars. They are seeking a skilled Propulsion Engineer to support the operation of engineering systems, focusing on design, development, and testing of prototype aircraft propulsion systems.
EnergyEnergy EfficiencyManufacturingWireless
Responsibilities
Troubleshoots, analyzes, and repairs systems in assigned area by utilizing standard engineering and scientific principles
Provides documentation and makes technical presentations as required
Must ensure traceability between system, subsystem and component level requirements
Directs the activities of designers, technicians and may direct the activities of less experienced professional staff
May represent the organization in providing solutions to technical issues associated with specific projects
Maintains the strict confidentiality of sensitive information
Performs other duties as assigned
Responsible for observing all laws, regulations, and other applicable obligations wherever and whenever business is conducted on behalf of the Company
Expected to work in a safe manner in accordance with established operating procedures and practices
Direct experience with aircraft propulsion engineering and systems, including gas turbine / internal combustion engine design and aircraft fuel and oil systems
Advanced knowledge of aircraft engine technology and systems, including turbofan, turboprop and turbojet engines
Advanced knowledge of aircraft propeller technology, including general working knowledge of theory and maintenance process
Ability to develop, document and release propulsion systems requirements
Direct experience with fast paced development process, especially aircraft propulsion system development and integration
Experience with detailed design, fabrication and qualification of engine Truss, Nacelle, firewall and critical propulsion system components
Ability to determine and validate propulsion testing instrumentations (i.e. fuel flow meter, pressure transducer, Thermo-couples and etc.)
Ability to use Engine Deck models to perform parametric study of engine performance with varying conditions
Ability to use IADS and other Data Acquisition software to collect and analyze data
Familiar with FEA analysis, thermal analysis, and Failure Modes and Criticality Analysis (FMECA)
Ability to manage supplier development, test and qualification activities
Understanding of military configuration control procedures and drafting standards
Experience with aircraft flight and ground testing with emphasis on technical report writing
Working knowledge of engine overhaul procedures and maintenance instructions
Qualification
Required
Typically requires a bachelor's degree, master's degree or PhD in engineering or a related technical discipline from an accredited institution and progressive engineering experience as follows; four or more years of experience with a bachelors degree or two or more years of experience with a masters degree. May substitute equivalent engineering experience in lieu of education
Must have a complete understanding of engineering concepts, principles, codes, and theory; experience demonstrating a broad application of those concepts; and, expanding knowledge of principles, concepts, theory, and practices in related technical specialties
Must possess the ability to understand new concepts quickly; apply them accurately throughout an evolving environment; organize, schedule, and coordinate work phases; and, determine the appropriate approach at the task level or, with assistance, at the project level to provide solutions to a range of complex problems
Must have excellent communication, computer, documentation, presentation, and interpersonal skills, ability to work independently and as part of a team; able to perform complex tasks in one engineering area; and, lead a team of less experienced professional employees on semi-routine tasks. Able to work extended hours as required
Ability to obtain and maintain DoD Security Clearance is required
Direct experience with aircraft propulsion engineering and systems, including gas turbine / internal combustion engine design and aircraft fuel and oil systems
Advanced knowledge of aircraft engine technology and systems, including turbofan, turboprop and turbojet engines
Advanced knowledge of aircraft propeller technology, including general working knowledge of theory and maintenance process
Ability to develop, document and release propulsion systems requirements
Direct experience with fast paced development process, especially aircraft propulsion system development and integration
Experience with detailed design, fabrication and qualification of engine Truss, Nacelle, firewall and critical propulsion system components
Ability to determine and validate propulsion testing instrumentations (i.e. fuel flow meter, pressure transducer, Thermo-couples and etc.)
Ability to use Engine Deck models to perform parametric study of engine performance with varying conditions
Ability to use IADS and other Data Acquisition software to collect and analyze data
Familiar with FEA analysis, thermal analysis, and Failure Modes and Criticality Analysis (FMECA)
Ability to manage supplier development, test and qualification activities
Understanding of military configuration control procedures and drafting standards
Experience with aircraft flight and ground testing with emphasis on technical report writing
Working knowledge of engine overhaul procedures and maintenance instructions
Preferred
Previous experience with engine cycle decks and ability to conduct parametric performance studies
Ability to configure and validate propulsion testing instrumentations (i.e., flow meter, pressure transducer, thermocouple etc.)
Experience with IADS and other data acquisition software to collect and analyze data
Experience with detailed design, fabrication, and integration of critical propulsion system components
Direct experience with aircraft propulsion engineering and systems, including gas turbine / internal combustion engine design and aircraft fuel and oil systems
Advanced knowledge of aircraft engine technology and systems, including turbofan, turboprop, and turbojet engines
Basic understanding and ability to run simple FEA analysis (ANSYS)
Basic understanding and ability to use either MATLAB, VBA, or similar for post processing
Company
General Atomics Aeronautical Systems
At General Atomics Aeronautical Systems, Inc.
Funding
Current Stage
Late StageTotal Funding
$6.76MKey Investors
US Department of Energy
2023-08-14Grant
2023-05-09Grant
2022-09-19Grant
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