This is a green propulsion thruster based on Nammo Hydrogen Peroxide technologies.

This is a green propulsion hybrid motor based on Nammo Hydrogen Peroxide technologies.

This spacecraft thruster has been developed for cold gas propulsion applications requiring a thrust between 10 mN and 100 mN.

The LEROS 1b is a high performance bipropellant chemical thruster, used for satellites and spacecraft.

The LEROS 1c is a high performance bipropellant chemical thruster.

The LEROS 2b is a high performance bipropellant chemical thruster.

The LEROS 2c is a high performance bipropellant chemical thruster.

The LEROS 4 is a high performance bipropellant engine for deep space missions. The engine can also be used for apogee insertion applications.

This high performance European 1N class Hydrazine monopropellant thruster has been developed and extensively proven by Nammo UK.

The Nucleus Sounding Rocket is designed and manufactured by Nammo Space at the Raufoss facility. Nucleus utilises the Andøya Space Centre Hotel payload module.

The Nammo Space Safe and Arm Device has been developed and qualified for use on the Ariane 5 and Vega launchers. It has also been used on the VLS and KSLV launch vehicles.

The Nammo Space solid rocket motor igniter has been developed for the Vega-C and Ariane 6 P120C engine, and is based on Nammo pyrotechnic heritage.