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.
Multi Burn Solid Rocket
TECHNOLOGY LICENSING OPPORTUNITY
technology Snapshot
Overview

Advantages
- Allows for complex flight maneuvers that require precise thrust modulation
- Combustion can be halted cleanly and then reinitiated
- Can place space vehicles in precise orbits for optimal performance
Problems Solved:
- Ignition system has been changed from one-time use to reusable
- Employs resettable mechanism to rapidly extinguish a burn
- Can be stored fully fueled for long periods of time
Market Applications
- Aerospace (i.e., Reusable Launch Vehicles)
- Defense and Military
- Commercial Satellites
- Space Tourism
On This Page
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