This 100ml 3D printed Titanium CubeSAT Tank has been developed for applications fitting inside the 1U envelope.

Nammo Space has responded to the growing requirement for demisable tanks required for small launchers and spacecraft.

The Apogee Engine Valve is a single stage, redundant solenoid coil thruster flow control device. It is a non-sliding fit valve, specifically designed for propulsion system applications.

The Dual In-line Chemical Thruster Valve is a two stage solenoid actuated non-sliding fit flow control device, designed for propulsion system applications.

This Nammo Space product is being developed for spacecraft propulsion systems where customers require precise pressure regulation or mass flow control.

The Fill and Drain Valve (FDV) or Fill and Vent Valve (FVV) is capable of sealing liquid propellant or gas and can be used in most spacecraft and launcher applications.

The well-established ‘SVS01’ is family of in-line Flow Control Valves which have been flying for more than twenty years. 

The In-line Flow Control Valve is a single stage solenoid actuated non-sliding fit flow control device, designed for propulsion system applications.

The Cold Gas Mechanical Pressure Regulator is a single stage passive flow control device, primarily intended for gaseous regulation in propulsion systems. The regulator will step down the high pressure inlet gas to a predefined outlet pressure for the customer.

This HTP CubeSat Fill and Drain Valve consists of a flight half and ground half coupling.

The Nammo Space Non-Return Valve is compatible with all standard propellants.