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Small Vehicle Experimental Launch Testbed (SVELT)

Completed TRL 2 (started at 2, targeting 2)

Description

The overall technical objective of the present study is to perform an engineering assessment of an F-4 aircraft with WIPCC to launch at supersonic speed a rocket-powered launch vehicle carrying a small payload

Benefits

Research to explore aircraft assisted launch capabilities

Details

Technology areaPropulsion Systems > Aero Propulsion
ProgramSmall Spacecraft Technology (SST)
Lead organizationAmes Research Center, Moffett Field, CA
Start date2011-08-01
End date2014-12-04

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.

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