The Thermal Engineering Branch is responsible for developing and applying technology to meet the thermal requirements of Goddard-managed spacecraft and space-borne scientific instruments. Some specific functions of the branch are listed below:

• Develop and integrate thermal control systems for spacecraft and instruments; verify resulting designs through analysis and environmental testing.
• Conduct vigorous research and development programs directed toward advancing the state-of-the-art in spacecraft thermal control technology; conduct laboratory and in-orbit test programs as required to demonstrate viability of these technologies in their intended applications.
• Provide technical oversight, evaluation, consultation, and support to flight projects, instrument developers, design review teams, failure analysis teams, technical evaluation panels, and source evaluation boards.
• Develop and assess thermal software packages. Develop software which fosters concurrent engineering practices.

For specific information, see our lists of:

• Groups: sections in the branch with specific responsibilites,
• Technologies: new methods and devices we are developing, and
• Projects: spacecraft, Shuttle payloads, and spacecraft instruments we have worked on.

New policies make it easier for us to work with other groups, both in and out of government. For more information, visit the Innovative Partnerships Program.