Bachar Elzein
CEO / Directeur Technique
Reaction Dynamics
Reaction Dynamics develops hybrid propulsion systems that enhance the efficiency and burn duration of rocket engines, addressing the limitations of traditional hybrid designs. Their Aurora launch vehicle offers dedicated launches at a lower cost, utilizing non-toxic solid fuel to minimize environmental risks during operations.
- Aerospace
- Hardware
Updated 7 months ago
Funding
Raised to date
$1.5MRaised to date based on public sources. This may differ from the amount the company actually raised and is based only on what is publicly available on the internet.
Funding rounds are not available yet.
Founders
Product
Problem
Traditional hybrid rocket engines face challenges in maintaining efficient combustion and achieving long burn durations, limiting their effectiveness for orbital launches and in-space propulsion. Furthermore, the use of cryogenic or toxic propellants increases operational complexity and environmental risks.
Solution
Reaction Dynamics develops advanced hybrid propulsion systems that overcome the limitations of conventional hybrid rocket engines. Their patented technology stabilizes the oxidizer-to-fuel ratio, enabling consistent, long-duration combustion for both launch and in-space applications. The Aurora launch vehicle provides dedicated launches for small satellites, utilizing non-toxic solid fuel to minimize environmental impact and enhance safety. Reaction Dynamics also offers green chemical thrusters for satellite mobility, including collision avoidance, orbit transfers, and deorbiting, using storable propellants for extended on-orbit life.
Target Audience
Reaction Dynamics targets small satellite operators seeking dedicated launch services, as well as satellite manufacturers and operators requiring efficient and reliable in-space propulsion solutions.
Features
- Patented hybrid rocket engine design for stable, efficient, and long-duration combustion
- Aurora launch vehicle offering dedicated launches with a 200kg payload to LEO and a 1.3m fairing diameter
- Non-toxic solid fuel eliminating pollutant release risks
- Green chemical thrusters for in-space propulsion with high-density impulse
- Micro Orbital Transfer Vehicle (OTV) for cubesat and smallsat mobility, fitting in a 12U form factor with >29,000 Ns total impulse
- Additive manufacturing techniques for intricate, mass-optimized engine geometries
- State-of-the-art test facility for rapid engine testing and design iteration
- Regenerative cooling enabling simplified engines using monolithic 3D printed components