The payload bay is 1.2 m in diameter and 2.5 m in length, providing a large volume available to accommodate the satellite(s).
This engine provides a maximum thrust of 100 kN with the ability to throttle down for precise orbit insertion. To be compliant with mission requirement and space debris policy, the engine can be reignited multiple times. It is equipped with a bell-shaped nozzle adapted to vacuum conditions.
The engine provides a maximum thrust of 700 kN. Combustion from HDPE/LOx propellants do not produce toxic fumes. The fumes are harmless for the inhabitants and wildlife surrounding the launching area. This booster stage engine is equipped with a bell-shaped nozzle to benefit from highest propulsive efficiency during ascent and atmosphere pressure variation.
The upper stage propel the payload to the targeted orbit. It is powered by a single engine. The upper stage is designed to be capable of delivering multiple satellites on different orbits and it deorbits itself after mission completion.
The booster propels the upper stage and its payload to the edge of space. It is powered by a single engine capable of 700 kN of maximum thrust. The booster is designed to modulate its thrust to reduce the intensity of the maximum aerodynamic pressure. After being jettisoned the booster stage dives back to Earth. It is reignited several times during reentry and for soft landing into the ocean.