Modular hybrid propulsion unit using solid HDPE fuel and N2O oxidizer for last-mile orbital maneuvers of small satellites — accelerates a 10kg payload to 1,100 m/s, 3D-printed manufacturing.
DARUMA Micro Hybrid Propulsion Unit
Modular hybrid propulsion unit using solid HDPE fuel and N2O oxidizer for last-mile orbital maneuvers of small satellites — accelerates a 10kg payload to 1,100 m/s, 3D-printed manufacturing.
Description
DARUMA Micro is Letara's hybrid propulsion unit, using solid HDPE (high-density polyethylene) fuel and N2O oxidizer, developed jointly with Hokkaido University's Laboratory of Space Systems. It targets rideshare satellites that need to travel beyond their drop-off orbit, supporting orbit transfers, orbital adjustment via integrated cold-gas nozzles and a re-ignitable main engine, and deorbit for debris removal or sample return missions. The system is manufactured using scalable 3D-printing techniques and supplied as a complete hardware set including combustors, piping, tanks, a simple CPU, and batteries, with optional exterior wall panels and attitude control devices.
Specifications
| Wet mass | 30 kg |
|---|---|
| Performance (10kg payload) | Accelerates to 1,100 m/s |
| Performance (100kg payload) | Accelerates to 400 m/s |
| Performance (300kg payload) | Accelerates to 130 m/s |
| Fuel | HDPE (high-density polyethylene) |
| Oxidizer | N2O (nitrous oxide) |
| Hardware included | Combustors, piping, tanks, simple CPU, batteries |
| Manufacturing | Scalable 3D-printing |
| Status | In development |