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Satellite Propulsion Systems - TerraSAR-X

Hydrazine reaction control system

 

TerraSAR - X satellite

TerraSAR-X

TerraSAR-X is the first satellite to be built in a Public Private Partnership in Germany. Here, the German Aerospace Centre (DLR) and Europe’s leading satellite system specialist Astrium have shared the cost of constructing and deploying the spacecraft.

The scientific exploitation of TerraSAR-X data will be conducted by DLR, while Infoterra GmbH, a 100% subsidiary of EADS Astrium GmbH, is responsible for the commercial marketing.

TerraSAR-X is a new generation, high resolution satellite operating in the X-band at 9.65 GHz that can operate independent of weather conditions, cloud coverage, and illumination and will be capable of delivering data at a resolution of up to 1 meter.

The continuous stream of remote sensing data from TerraSAR-X will support numerous scientific and commercial applications. In Germany the TerraSAR-X Project is borne by a broad science community. The satellite will provide unique data, leading to new applications and methods in geosciences, as there are in the solid earth's physics. This includes the observation of minor tectonic shifting, in hydrology the modelling of catchment areas, in climatology the quantifying of global biomass and changes in oceanography, the ice coverage of the poles.

The data/products of TerraSAR-X will also be used to support public interests and the performance of governmental tasks such as environmental monitoring (contribution to the EU's GMES-Programme), air traffic, mobile telecommunication services, regional planning (provision of large scale topographic maps) and civil protection support, with high resolution data.

TerraSAR-X will operate for at least 5 years and will carry an active X-band instrument. Customarily, it is necessary to turn a satellite in order to obtain a different viewing angle. TerraSAR-X, however, has moving "eyes" that enables a scanning path to be swathed by active antenna. The extensive data streams will be transmitted to Earth via broadband technology.

On 15th June 2007, the 1200 kg satellite was successfully launched from Baikonur, Kasachstan using a DNEPR-1 launcher placing TerraSAR-X into a 514-km polar orbit. As the Earth rotates below this orbit, the satellite will scan all regions of the Earth swath by swath. Priority observations of any site can be performed within three days.

Just four days after launch, TerraSAR-X provided the first brilliant satellite images.

 

Reaction Control System
Astrium Lampoldshausen was responsible for the design, development and production of the TerraSAR-X monopropellant hydrazine Reaction Control System (RCS).

TerraSAR-X Reaction Control System Configuration

Reaction Control System Configuration

 

In designing the RCS, the major requirement was for the use of existing space qualified components to the greatest extent possible. This requirement was fulfilled by using components previously used on the GLOBALSTAR programme, thereby inheriting the reliability and low cost requirements.

 

Astrium Lampoldshausen responsibilities included:

Manufacturing, Assembly, Integration and Test of the complete RCS.

Participation during the RCS integration into the satellite at EADS Astrium GmbH, facilities

Participation and support during satellite system testing.

 

The RCS comprises:

Eight 1N thrusters, model CHT-1

One propellant tank, model OST-32

Two fill & drain/vent valves

One set of Tubing with brackets

 

Modular Propulsion Systems Design
The complete Reaction Control System is designed for pre-assembly into compact functional modules at Astrium Lampoldshausen complete with interfaces exactly matching that of the spacecraft. All pipework is also precisely pre-formed and assembled into kits at Lampoldshausen.

The modular integration of spacecraft propulsion systems was pioneered at Astrium Lampoldshausen and provides the following advantages:

Propulsion module can be acceptance tested, including high pressure proof testing and functional verification at Lampoldshausen, before delivery to customer facilities.

Minimises GSE required at customer facilities.

Simplification of final integration to the spacecraft.

Minimises propulsion integration time at the customer facilities.

These advantages have been proven over again on numerous spacecraft. Pre-integration of the propulsion module at Lampoldshausen minimises direct access to the spacecraft to just a few days for final integration and test.

 

Image Gallery: TerraSAR-X Reaction Control System

 

Hydrazine propulsion module integration at EADS Lampoldshausen

Propulsion Module Integration
at Astrium Lampoldshausen

 

Two hydrazine thruster clusters each with 4 x 1 N thruster

Two Thruster Clusters
(4 x 1.0 N thrusters each cluster)

Completely pre-integrated hydrazine propulsion module at EADS Lampoldshausen

Complete, Pre-Integrated Propulsion
at Astrium Lampoldshausen

 

 

Hydrazine propulsion module ready for delivery to customer facilities

Propulsion Module ready for delivery
to customer facilities

Modular element ready for integration at customer facility

Modular Element ready for Integration
at customer facility

 

 

Integration of modular hydrazine element to TerraSAR-X

Integration of Modular Elements to TerraSAR-X

Modular element integrated to TerraSAR-X

Modular element integrated to satellite

 

 

Preparation of hydrazine tank module

Preparation of Tank Module

Hydrazine tank module integrated to TerraSAR-X

Tank Module integrated to satellite

   



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