Executing all necessary phases of projects while prioritizing the safety and efficiency of space platforms such as satellites, orbit transfer vehicles, and launch systems, based on specified engineering requirements.
Having knowledge of reusable launch systems and propulsion systems based on sustainable aviation fuels.
Analyzing components in high-vibration and high-pressure environments.
Designing subsystems and equipment deemed necessary for conducting system-level tests.
Conducting studies on the material behaviors of various materials at cryogenic and high temperatures in the development of launch vehicle systems.
BASIC QUALIFICATIONS:
Bachelor's degree in Aeronautical Engineering, Aerospace Engineering, Mechanical Engineering, Mechatronics Engineering, Metallurgy and Materials Engineering, or Chemical Engineering from a university.
Experience with the use of any 3D CAD software (preferably CATIA V5/V6, etc.).
Ability to use computational engineering support applications at a basic level (preferably Ansys, MATLAB, Python, COMSOL, ABAQUS, LabVIEW, PTC Creo).
PREFERRED SKILLS AND EXPERIENCE:
Knowledge of hazardous systems (high pressure, high energy, hazardous liquids/gases, cryogenic, hypergolic, pyrophoric fuels) and measures to prevent potential dangers.
Familiarity with manufacturing methods and processing techniques, additive manufacturing, forging, casting, shaping, heating, ventilation, air conditioning, coating, non-destructive testing, heat treatment, leak testing, thermal control paints, and laser/plasma cutting and bending.
Acquaintance with instrumentation and control components (pressure transducers, thermocouples, RTDs, strain gauges, accelerometers, flowmeters, load cells, relays, solenoids, pneumatic valves).
Experience in combustion chamber design, analysis, manufacturing, testing, and engine ignition.
Experience in the design and production of propellant gases and gas systems.