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LEAP 71

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We create computational models for engineering to build the world's most advanced machines.

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Our first aerospike rocket thruster. 5 kN (1,125 lbf) kerolox. Aerospikes are among the hardest rocket engines to develop. Few teams have successfully hot-fired liquid-propellant versions, and none has yet flown to space. Although the geometry is radically different from a conventional bell nozzle, the governing physics are the same. That makes aerospikes an ideal fit for Noyron, which generates engines from underlying physical principles rather than from CAD drawings. An aerospike turns the conventional nozzle inside out. Its toroidal geometry eliminates the fixed outer bell wall, which forces a conventional thruster to choose one atmospheric regime. A sea-level bell nozzle sacrifices performance at high altitude. A vacuum-optimized nozzle cannot be operated safely at sea level. Aerospikes are efficient under all atmospheric conditions, making them highly relevant for reusable upper stages that fly back from space to the launch site. Cooling them is the biggest challenge. Our engine uses liquid oxygen to regeneratively cool the inner spike and kerosene fuel to cool the outer shroud. The resulting warm LOX gives the engine a nice Isp boost. We hot-fired this engine in December 2024. Its early success encouraged us to pursue aerospikes as a parallel track across our engine programs.

Our first aerospike rocket thruster. 5 kN (1,125 lbf) kerolox. Aerospikes are among the hardest rocket engines to develop. Few teams have successfully hot-fired liquid-propellant versions, and none has yet flown to space. Although the geometry is radically different from a conventional bell nozzle, the governing physics are the same. That makes aerospikes an ideal fit for Noyron, which generates engines from underlying physical principles rather than from CAD drawings. An aerospike turns the conventional nozzle inside out. Its toroidal geometry eliminates the fixed outer bell wall, which forces a conventional thruster to choose one atmospheric regime. A sea-level bell nozzle sacrifices performance at high altitude. A vacuum-optimized nozzle cannot be operated safely at sea level. Aerospikes are efficient under all atmospheric conditions, making them highly relevant for reusable upper stages that fly back from space to the launch site. Cooling them is the biggest challenge. Our engine uses liquid oxygen to regeneratively cool the inner spike and kerosene fuel to cool the outer shroud. The resulting warm LOX gives the engine a nice Isp boost. We hot-fired this engine in December 2024. Its early success encouraged us to pursue aerospikes as a parallel track across our engine programs.

15,519 Aufrufe

Our 20 kN MethaLOX bell-nozzle engine post hot-fire. This engine was generated by the same Noyron Computational Engineering Model as our aerospike. The engines look entirely different but are simply two expressions of the same thruster DNA.

Our 20 kN MethaLOX bell-nozzle engine post hot-fire. This engine was generated by the same Noyron Computational Engineering Model as our aerospike. The engines look entirely different but are simply two expressions of the same thruster DNA.

57,141 Aufrufe

Noyron allows us to design complex machinery and iterate at unprecedented speeds. Experimentation is the mother of innovation. CAD-based workflows penalize iteration, whereas computational models allow us to be even playful with the design of complex objects.

Noyron allows us to design complex machinery and iterate at unprecedented speeds. Experimentation is the mother of innovation. CAD-based workflows penalize iteration, whereas computational models allow us to be even playful with the design of complex objects.

15,283 Aufrufe

Made in Dubai. We printed this 200 kN MethaLOX Aerospike rocket engine with HBD out of Inconel 718. The refined version of this thruster will power the fully reusable upper stage of the Oryx spacecraft made by Aspire Space.

Made in Dubai. We printed this 200 kN MethaLOX Aerospike rocket engine with HBD out of Inconel 718. The refined version of this thruster will power the fully reusable upper stage of the Oryx spacecraft made by Aspire Space.

18,536 Aufrufe

20 kN cryogenic methane / liquid oxygen rocket engine ready to fire. Generated autonomously in a matter of hours by the Noyron Large Computational Engineering Model. Metal 3D-printed in copper (CuCrZr). From pure spec to test in less than 3 weeks.

20 kN cryogenic methane / liquid oxygen rocket engine ready to fire. Generated autonomously in a matter of hours by the Noyron Large Computational Engineering Model. Metal 3D-printed in copper (CuCrZr). From pure spec to test in less than 3 weeks.

22,796 Aufrufe

Sub scale version of our hypersonic precooler - generated from the same Noyron DNA as the large 1.5m version we printed with Farsoon.

Sub scale version of our hypersonic precooler - generated from the same Noyron DNA as the large 1.5m version we printed with Farsoon.

25,670 Aufrufe

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