Electra.aero · 3 months ago
Staff Design Engineer - Propulsion
Electra.aero is pioneering sustainable aviation by developing hybrid-electric aircraft designed to transform regional air mobility. The Staff Design Engineer - Propulsion will conduct design, analysis, test, and integration of propulsion systems for Electra's eSTOL aircraft.
AerospaceAir TransportationElectric Vehicle
Responsibilities
Complete designs for mechanical integration of propulsion systems utilizing NX CAD modeling and analysis tools
Working with suppliers as necessary to mechanically integrate components into the airframe
Knowledge of and experience working with and designing to FAA Part 23 structural requirements and derived ASTM standards
Managing physical interfaces between propulsion components and the airframe
Complete trade studies on alternative designs to meet requirements and objective functions
Performing modeling, analysis and simulation (eg static and dynamic stress analysis) to verify integrated propulsion components meet performance and safety requirements
Preparing and presenting at gated design reviews to demonstrate the adequacy of the design
Communicating information about propulsion integration design, requirements, and performance between the design team, management, customer, subcontractors, and vendors
Qualification
Required
Minimum of 2+ years of experience in mechanical engineering on air vehicles with bachelor's degree in mechanical engineering (or related STEM discipline)
Experience in aerospace component design
Understanding of manufacturing methods (machining, sheet metal, composites, 3D printing, injection molding, composite lamination, etc)
High competence with, and fluid use of, engineering first principles
A strong work ethic and ability to independently meet and lead the areas described by the responsibilities and essential functions
Excellent organization and communication skills
Complete designs for mechanical integration of propulsion systems utilizing NX CAD modeling and analysis tools
Working with suppliers as necessary to mechanically integrate components into the airframe
Knowledge of and experience working with and designing to FAA Part 23 structural requirements and derived ASTM standards
Managing physical interfaces between propulsion components and the airframe
Complete trade studies on alternative designs to meet requirements and objective functions
Performing modeling, analysis and simulation (eg static and dynamic stress analysis) to verify integrated propulsion components meet performance and safety requirements
Preparing and presenting at gated design reviews to demonstrate the adequacy of the design
Communicating information about propulsion integration design, requirements, and performance between the design team, management, customer, subcontractors, and vendors
Preferred
Experience with mechanical system design and integration for certification to part 23 or 25 standards
Demonstrated knowledge of the Federal Aviation Regulations (FARs), certification procedures (especially Part 23), and relevant industry standards
Experience in Siemens NX CAD Software and Teamcenter PLM Software
Competency in engineering analysis, including structural, thermal, multi-body dynamics, and electrical
US Person (Citizen or Green Card) Preferred
Benefits
Medical
Dental
Vision
STD
LTD
Life insurance
Generous PTO and sick leave
Company holidays
Paid winter break
401(k) plan with immediate vesting
Free catered lunches
Amazing coffee
Snacks
Drinks
Fruit
Free parking
Company
Electra.aero
Electra develops hybrid-electric aircraft for sustainable urban and regional air mobility.
Funding
Current Stage
Growth StageTotal Funding
$115MKey Investors
Prysm CapitalStatkraft VenturesVirginia Innovation Partnership Corporation
2025-04-21Series B· $115M
2023-07-26Series Unknown
2023-06-01Grant
Recent News
2025-11-24
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