← Back to NASA Technology Projects

Damage-Tolerant, Lightweight, High-Temperature Radiator for Nuclear Powered Spacecraft, Year 2

Completed TRL 2 (started at 1, targeting 2)

Description

Game-changing propulsion systems are often enabled by novel designs using advanced materials. Radiator performance dictates power output for nuclear electric propulsion (NEP) systems. A model developed at UMass showed that use of novel materials and designs for a high-temperature radiator for space-based power systems can dramatically improve the power per weight and weight per area.

Benefits

It will provide a more detailed, predictive modeling capability in order to help guide design efforts for radiators.

Details

ProgramCenter Innovation Fund: MSFC CIF (MSFC CIF)
Lead organizationMarshall Space Flight Center, Huntsville, AL
Start date2012-10-01
End date2013-11-01

Project contacts

Listed on TechPort itself — the most direct way to ask about this specific project.

How to get involved

This is early/mid-stage (TRL 2) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.

None of these are guaranteed paths for this specific project — TechPort itself doesn't have an "apply" button. Reaching out to the contact(s) above with a specific question is usually the fastest way to find out what's actually open.