Noyron RP
A Computational Engineering Model
for Space Propulsion

Noyron RP is a specialized computational model for designing rocket propulsion systems. It is based on the Noyron Large Computational Engineering Model.

Noyron RP produces a variety of spacecraft components and integrated systems, including injector heads, traditional bell-nozzle type combustion chambers, as well as advanced engines such as aerospike.

The Computational Engineering Model (CEM) uses analytical thermal and thrust models, heuristics, and condensed aerospace engineering logic, all encoded in a coherent algorithmic framework.

Noyron RP allows engineers to go from abstract input specifications such as propellant types, desired thrust, chamber pressure, to a manufacturable engine geometry in minutes. Through a wide set of parameters, designs can be iterated on, physical simulation results fed back, as well as actual testing data, to quickly converge on a validated engine prototype.

LEAP 71 is conducting it’s own tests and is working with partners on the physical validation of the designs generated by Noyron. We collaborate with the world’s leading Additive Manufacturing companies to ensure manufacturability.

Contact us for more information.