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Modular Propellant Storage


High-Performance, scalable propellant tank systems designed specifically for CubeSats. Engineered for green propellants, built with integrated structural mounting, and fully customizable with mission-specific Propellant Management Devices.

From agile 1U platforms to larger CubeSat missions - our modular propellant tank solutions deliver safe handling, efficient propulsion, and seamless spacecraft integration. Compliant with modern launcher requirements.


Dry mass
Starting from 200g


Material
Space graded Stainless Steel and Aluminum


100%
ITAR Fee



Volume
Starting from 1U


Pressure
Rated for green propellants


Propellant management device
Engineered for Propellant and Tank size


Valve Portfolio


Solenoid Valves
Our electromagnetic solenoid valves provide dependable, leak-tight isolation and precise flow control. Available in both monostable (normally closed) and bistable latching configurations. They enable flexible system architectures ranging from fast-response safety isolation to ultra-low-power long-duration missions.

Check Valves
Our check valves ensure safe and stable propellant flow without the need for power or active control. Engineered for minimal pressure drop and exceptional sealing performance, they prevent backflow, protect sensitive propulsion components and maintain system integrity throughout the mission lifecycle.

Pressure Relief / Safety Valves
Our pressure relief and safety valves are designed to protect propulsion systems during ground operations, integration, and testing. They provide reliable over-pressure protection during propellant filling, transport, and handling. Ensuring safe workflows throughout the spacecraft preparation and qualification process.


Propulsion Avionics


Our propulsion avionics are specifically designed to meet the size, power and integration constraints of CubeSat missions. Acting as the central control unit for satellite subsystems. They provide reliable valve actuation, temperature management and continuous monitoring of critical system parameters such as pressure and thermal conditions.

The modular architecture allows the system to grow alongside mission requirements - from lightweight single-string configurations for small CubeSats to more advanced setups with expanded telemetry channels and configurable redundancy. This ensures an optimal balance between performance, mass, and power consumption for every mission class.


Communication
CAN-BUS / RS485


Single-Point
Interface between Spacecraft and Propulsion System


100%
ITAR Free


Redundancy
Scalable


Radiation
Tolerant or hardened


Space-grade
manufactured