This propulsion system enables multiple independently controllable impulses from a single solid rocket while maintaining the high thrust, safety, simplicity, reliability, scalability, and storability of traditional solid rockets.
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Published: 2025-08-04
LA-UR-25-26225
Application Area
Sectors:Aerospace & Defense Systems
Markets:Aerospace, Defense, Comercial Satellites, Space Tourism
Technology Readiness Level:
4 - Component Prototypes Tested in a Controlled Environment
IP Information
Patent Number: 11,859,579-B1
S Number: S-133685
Contact
- Licensing
- Los Alamos National Laboratory
- licensing@lanl.gov
