From airplanes to spaceships, flying technology requires an incredible amount of skill and precision to design and keep working. Lives depend on it being done properly, and that is where the incredibly skilled aerospace engineering steps forth to get the work done and guide the technology to the future.
How to Become a Successful Aerospace Engineer?
All work in this field requires a very high amount of education, training, and experience to succeed. A bachelor’s, master’s, or a PHD will be required by employers, along with all necessary training to pass any particular license programs required by the state or your particular employer to prove you have the skills.
Where you work will affect what kind of work to expect. NASA puts most of its energy into space travel or satellites for research, while the army will mostly be developing new fighter jets and surveillance equipment for combat. A more general airplane developer will work on commercial jets for transportation.
Being incredibly focused on detail and getting your calculations right is a must in this field, as a miscalculation or a sloppy detail can quite literally risk lives. You will always want to be vigilant for your own mistakes as well as the errors of others, as catching them will save everyone involved in the long run.
Working well with a team is a must for big jobs, and designing such massive machines requires quite a few people. You will want to work with everyone and always look for ways the process can be improved, as the field of air travel is always evolving and looking for the next big idea.
The Best Aerospace Engineer Resume Samples
These are some examples of job descriptions we have handpicked from real Aerospace Engineer resumes for your reference.
- Prepared detailed engineering specifications for broad and complex projects and repairs involving aircraft systems or airframe components.
- Provided engineering assistance to all customers who require support in such areas as Service Bulletins and Alert Directives.
- Responsible for directing, coordinating, designing, and preparing major modifications resulting in Supplemental Type Certificates.
- Improved efficiency and streamlined processes to reduce costs by creating reusable analysis spreadsheets and creating reports/memos that can be referenced for similar analyses.
- Coordinated with other departments for the F-16 Report Maintenance project by requesting numerous documents to be uploaded on EDMS to ensure easy reference throughout the group.
- Updated flight manual procedures to better identify aircraft capabilities based on stores carriage configurations for multiple countries.
- Involved in creating demonstrations of a state of the art strain sensing system.
- These are designed to highlight the response of interesting structures to static stresses, dynamic thermal inputs, and vibration environments.
- Live demos are broadcast continuously, with high-speed real-time data from 4000 strain gauge sensors embedded in a fiber optic cable.
- Created Engineering Equivalency and Concurrence documents for Regional Airline clients.
- Provided exclusive project management for AOG and non-AOG turn-key aircraft repair solutions for business jet owner/operator clients.
- Responsibilities included repair design and analysis, coordination with Part 145 Repair Facilities, MRO partner companies, FAA DERs, and shipping/logistics back to clients.
- Mentored and developed junior engineers and established company engineering learning tools.
- Provide technical guidance for updates to Safety Requirements documents as well as provide technical direction/interpretation when necessary.
- Coordinate various meetings to resolve issues and/or attain program direction as needed for various high-level projects.
- Develop written and/or oral reports in order to provide technical briefings, activity summaries, review notes, etc.
- Delivered meshed composite panels of Airbus A350 XWB aircraft using Hypermesh in very limited time with good quality for non-linear FE crash test.
- Collaborated with designers to identify the critical geometry changes of Airbus A321 Aircraft which impacts the strength of the structure.
- Assisted in ISAMI analysis of Airbus A350XWB composite panel bolted joint analysis.
- This was anchored with the above cryogenic testing for edification as well as future design changes.
- Procured redundant, brushless DC motor with redundant resolver position sensors.
- Designed and analyzed panel that accepted the FCV along with Marotta Valves, thermocouple measurements, mixer, and check valves.
- Led program team through requirements development and industry research.
- Assimilated input from 10 industry partners while coordinating expectations from multiple Air Force customers.
- Planned acquisition strategy and developed broad agency announcement.
- Responsible for coordinating and driving the status of Validation and Verification activities on the nacelle system program & technical activities.
- Interface with customers and internal engineering personnel for the purpose of communicating technical information.
- Generate reports suitable for transmittal Airworthiness and Customer.
- Managed the development of innovative aerospace propulsion systems, from concept definition through prototyping & testing.
- Oversaw the full development life-cycle of cutting-edge solid divert & attitude control thrusters as well as planning, budgeting & interfacing with suppliers/customers.
- Led the design and procurement efforts on the development of a ground-breaking hybrid rocket motor providing over 70,000 lbf. of thrust.
- Provided multi-disciplinary engineering support for the proposal efforts for new business opportunities including system analysis, conceptual design, cost analysis and more.
- Perform aerodynamic analysis & stress analysis of conceptual and prototype air vehicles.
- Size, design, and manufacture proof-of-concept models and prototypes.
- Generate and execute test & evaluation procedures during manufacture, static test, and flight test phases of development.
- Draft patents and presentations for a portfolio of conceptual, proof-of-concept, and flying prototype vehicles.
- Recalculate fastener joint stiffness, during repairs due to that the fasteners are oversize therefore the fastener stiffness changes, which requires re-calculation.
- Level 2 Fatigue Crack Initiation Life (CIL) Assessment for Wings, ensuring the structural repairs meet the extended component life goals of 10,000 flight hours.
- Review and approve the structural repair analysis from local analysist and contractors to ensure the analysis and repair is structurally capable for any fleet mission.