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Hydrazine Thrusters

Thruster Introduction
1 N Thruster
20 N Thruster
400 N Thruster
Heritage Thrusters

Airbus Space Systems Hydrazine Thrusters

Thrusters for satellites, spacecraft, space probes and launch vehicle attitude control.

1N EuroValve hydrazine thruster.

Airbus Space Systems, Lampoldshausen first engaged in hydrazine propulsion technologies in 1966. Since that time, the Centre has become an international leader in the development, production and testing of hydrazine thrusters and propulsion systems for commercial, scientific and military spacecraft.

Thrust Range

Since 1966, a wide range of thrust levels were required for the many different programmes. Today, the thruster range has been rationalised to the more frequently demanded 'work horse' thrusters with the benefit of a consistent production line type manufacturing process. The units currently available are the 1 N, 20 N and 400 N thrusters.


Heritage thrusters, that are no longer produced are included here for completeness and reference purposes.

General Description

Our hydrazine thrusters use storable monopropellant N2H4. Thrust is produced by the decomposition of hydrazine as it passes through a catalyst bed.


Thrusters are designed for operation in both steady state and pulse mode operation over a wide pressure range and are thus ideal for propulsion systems operating in blow-down mode.


All thruster combustion chambers and nozzles are manufactured from Haynes 25 alloy. The thruster structure is also designed to serve as a heat shield for protecting the propellant valve and spacecraft structure.


Thrusters are equipped with an internally redundant catalyst bed heater and thermal insulation to guarantee optimum reproducible start-up conditions. Moreover, our thrusters are qualified for multiple cold starts.


Thruster valves are of the dual seat solenoid type, produced by Airbus Space Systems and also by external partners. The nominal valve voltage is 28 Volts DC. Thruster performance is identical for both valve types.

Thrust Levels

Our flight qualified hydrazine thrusters range from 0.5 N to 400 N nominal thrust. The 'work horse' thrusters selected for the majority of programmes are the 1.0 N, 20 N and 400 N thrusters.


Hydrazine thruster assembly area.
Hydrazine thruster assembly facility

Customarily, all of our hydrazine thrusters are adapted to specific customer requirements. We supply from thruster and component level through to complete plug-in propulsion modules. Both thruster and complete propulsion systems can be operated over a wide pressure range in both pressure regulated and system blow-down modes.

Propulsion Module

Many of our complete hydrazine propulsion systems are supplied as self contained 'plug-in' propulsion modules. The module, comprises the complete propulsion system together with all of the associated sensors, heaters, thermistors, pressure transducers and harness elements.


The 'plug-in' propulsion module provides just two interfaces to the spacecraft:


  • A structural interface to the spacecraft.
  • A single electrical interface via connectors.


Further details of a typical plug-in propulsion modules can be found in the Rocsat 2 page.

Launch Vehicle Applications

Our hydrazine thrusters are also used for launch vehicle roll control and upper stage orientation and precision manoeuvres, as used on the Ariane 5 launcher.

Thruster Availability

Thrusters in high demand are economically produced on a series production line and are therefore readily available, subject to customer specific requirements. Thrusters with less demand are made to order.


Hydrazine Thruster Brochure (PDF)

PDF Brochure -Hydrazine Thrusters


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