Indian startup Othisis has conducted a stationary test-fire of its first 3D-printed, fully cryogenic rocket engine prototype. This marks a significant step for the two-year-old company, founded by Syed Affan.
The unnamed engine is a 5 kN design that utilizes both liquid oxygen (LOX) and methane as propellants, kept in a chilled liquid state. Othisis intends this design for Vertical Take-off, Vertical Landing (VTVL) reusable applications. The design incorporates a chilled-fuel loop for cooling.
Methane and LOX propellants offer a stronger burn than Kerolox and produce almost no residue, which can lower maintenance time and improve reusability turnaround. Both LOX and methane can theoretically be manufactured in-situ from CO2 and water. However, drawbacks include lower fuel density requiring larger tank sizes, trickier storage due to low temperatures, and potential handling hazards.
The engine was manufactured using Selective Laser Melting (SLM) 3D printing. This process involves depositing layers of microscopic metal powder and melting them with a laser, creating layers approximately 0.05 to 0.06 mm thick. SLM allows for the use of metals and alloys not typically handled by consumer 3D printers, enabling complex designs for rocket components.
Despite being a relatively new company, Othisis has reportedly signed Memorandums of Understanding (MoUs) to carry payloads into space. This indicates early industry interest in their propulsion technology.
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Indian startup Othisis successfully test-fired a 3D-printed, 5 kN fully cryogenic rocket engine prototype. This development demonstrates the potential of Selective Laser Melting (SLM) 3D printing for manufacturing advanced rocket propulsion systems, which could impact the cost and efficiency of space launches.