This position provides leadership in thermal design, analysis, and test support of various NASA Space System projects such as:

Human Landing System (HLS) to deliver American astronauts the first woman and next man on the Moons south pole

International Space Station (ISS) environmental variables controls, and experimental payloads thermal/fluids support

Space Launch Systems (SLS) Avionics Thermal/Fluids support

Ground Support and Test Equipment

Spacecraft Thermal/Fluids support

Job Requirements:

A degree in Mechanical, Chemical, or Aerospace Engineering or related field with at least 2 years of experience is required. A degree from an ABET accredited university is preferred.

The Successful candidate shall have:

Proficiency with thermal test set up support, Excel, PowerPoint, and Word

Experienced in thermal desktop code and thermal testing

Deep understanding/ knowledge of orbital thermal environment development

Excellent written and verbal communication skills

Familiarity with NASA standards and MSFC Specifications

Experience with leading engineering teams