Combustion Engineer II/III

Firehawk Aerospace is in search of an accomplished Combustion Engineer to take the contribute in advancing hybrid rocket propulsion systems. As a pivotal contributor, you will operate at the cutting edge of technology, spearheading the design, testing, and enhancement of combustion processes vital to our national defense and space exploration endeavors. This role presents an opportunity to drive innovation and make a significant impact in the field of aerospace propulsion.

Responsibilities:

• Participate in the design and analysis of combustion chambers, injectors, and associated components of hybrid rocket engines and other propulsion devices
• Apply advanced computational tools and simulations to optimize combustion performance under various operating conditions
• Evaluate and develop hybrid rocket engine propellants, ensuring compatibility with combustion systems and achieving desired performance characteristics
• Plan, execute, and analyze combustion tests to assess performance, stability, and efficiency
• Continuously improve combustion system efficiency, stability, and safety while meeting project goals and objectives
• Work closely with multidisciplinary teams, including propulsion engineers, materials scientists, and systems engineers, to integrate combustion systems into complete rocket propulsion systems
• Maintain accurate and detailed records of designs, test results, and simulations
• Prepare technical reports and presentations for internal and external stakeholders
• Stay up-to-date with the latest advancements in hybrid rocket propulsion technology and combustion theory

Basic Qualifications include:

• Experience in combustion modeling, testing, and analysis
• Proficiency in reading and interpreting Piping and Instrumentation Diagrams (P&ID)
• Working knowledge of office and productivity software (Office, JIRA, Confluence, etc)
• Working knowledge of relevant specialty software, such as- Fluent, Creo, and Windchill
• 5 years or more years of engineering experience
• Ability to mentor and lead less experienced engineers
• Ability to travel as needed to support testing
• Eligibility to work in ITAR/EAR environments
• Must meet ITAR requirements

Preferred Qualifications:

• 5 years or more years of engineering experience in aerospace fluid systems
• Direct experience with designing and testing engines, gas turbines, or rocket engines
• Direct experience with designing and testing fuel injectors and nozzles.
• Working knowledge of hybrid engines
• Experience in hybrid engine combustion analysis
• Advanced degree in mechanical or aerospace engineering or science based field
• Proficiency in fluid and pressure systems design
• Working knowledge of various programming languages (Fortran 90, Python, MATLAB)
• Active or Previous Security Clearance