FULL ACTIVE THRUST CONTROL
HIGH SPECIFIC IMPULSE
MULTIPLE HYPERGOLIC IGNITIONS
Advanced space systems require precision maneuverability with powerful performance.
Our unique bi-propellant is hypergolic. The ignition is created spontaneously once the fuel and oxidizer stream into the engine. This allows our engines
to be fully controllable with numerous on/off ignitions, which is exactly what's needed for spacecraft or satellites for maneuvering in space.
GREEN HYPERGOLIC FUEL
NewRocket uses a special bi-propellant composed of our gel state proprietary fuel and an oxidizer. Legacy highly toxic bi-propellants are mostly based on Hydrazines, thus creating significant safety risks and driving high operational costs. Our unique PowerGel allows simple, safe, flexible and cost effective storage and operation, leading to a significant reduction in overall mission costs.
SHORTER DEVELOPMENT TIME
FROM SINGLE TO THOUSANDS OF NEWTONS
We are developing a range of rocket engines starting from single Newtons to thousands of Newtons of thrust levels. For example, our 400N thrust class engine which is a perfect fit for demanding space applications such as space tugs, landers and other in-space maneuvering applications.