← Back to NASA Technology Projects

Light weight composite Payload Fairing development

Completed TRL 3 (started at 2, targeting 4)

Description

Develop lightweight high performance sandwich composite structure for launch vehicle payload fairing requiring no thermal protection system (TPS),

Benefits

Elimination of TPS leads to structure weight savings and Improvement in component quality by having less processing steps

Details

Technology areaMaterials, Structures, Mechanical Systems, and Manufacturing > Materials > Lightweight Structural Materials
ProgramCenter Independent Research & Development: MSFC IRAD (MSFC IRAD)
Lead organizationMarshall Space Flight Center, Huntsville, AL
Start date2020-01-01
End date2020-12-31

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 3) — 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.