Senior Thermal Engineer

Application close date:

Applications will be accepted on an ongoing basis until the requisition is closed.

This role supports the development and operations of New Glenn, a single-configuration, heavy-lift orbital launch vehicle capable of routinely carrying people and payloads to low-Earth orbit, geostationary transfer orbit, cislunar, and beyond. Its first stage is fully reusable, and the vehicle was designed from the beginning to be human-capable.

As part of a small, passionate and accomplished team of engineers and analysts, you will support thermal and fluid system design across New Glenn spaceflight systems. You will share in the team's impact on these systems across their full lifecycle, from early concept and configuration through flight operations and sustaining engineering. 

This role is analysis-intensive: you will integrate customer-provided payload thermal models and generate thermal predictions for payloads and the payload compartment during launch and ascent, while supporting analysis across all phases of flight. This work includes applying aerothermal, radiative, and natural environments to integrated vehicle thermal models. As the focal point for thermal analysis requests from customers and multiple internal teams, you will define analysis scope, assumptions, and deliverables, and deliver integrated thermal analyses that drive design, verification, and mission decisions. You will build, maintain, and configuration-manage integrated thermal models, inputs, and results, and document your analyses in formal reports and data books. You will also review and critique models and results produced by other engineers and mentor junior team members.

We are looking for someone who will apply technical expertise, leadership and a commitment to quality to positively impact safe human spaceflight. Passion for our mission and vision is required!

Minimum Qualifications:   

• Minimum of BS degree in Mechanical or Aerospace Engineering

• 5 or more years of experience in the fields of thermal or thermodynamic analysis

• Demonstrated expertise with Thermal Desktop and SINDA/FLUINT

• Demonstrated experience developing integrated thermal models of space or launch vehicles

• Experience reviewing and critiquing models and results developed by junior engineers

• Must be a U.S. citizen or national, U.S. permanent resident (current Green Card holder), or lawfully admitted into the U.S. as a refugee or granted asylum.

Preferred Qualifications:  

• MS or PhD degree in Mechanical or Aerospace Engineering

• 10 or more years of experience in the fields of thermal or thermodynamic analysis

• Demonstrated expertise with ANSYS Mechanical APDL

• Experience analyzing satellites, spacecraft, and/or launch vehicle upper stage systems

• Experience with payload integration, including payload thermal model exchange and interface requirements

• Demonstrated ability to automate analysis workflows using MATLAB and/or Python, with Git for version control

• Working knowledge of 3D CAD tools (Creo preferred)

Base Pay Range for:

CO applicants is $133,500.00 - $186,898.95 WA applicants is $145,188.00 - $203,263.20

Other site ranges may differ

Benefits

• Benefits include:  Medical, dental, vision, basic and supplemental life insurance, paid parental leave, short and long-term disability, 401(k) with a company match of up to 5%, and an Education Support Program.
• Stock Options for all regular employees (working at least 20 hours/week)
• Paid Time Off:  Up to four (4) weeks per year based on weekly scheduled hours, and up to 14 company-paid holidays.
• Dependent on role type and job level, employees may be eligible for benefits and bonuses based on the company's intent to reward individual contributions and enable them to share in the company's results, or other factors at the company's sole discretion. Bonus amounts and eligibility are not guaranteed and subject to change and cancellation. Please check with your recruiter for more details.