TanDEM-X
Formation flying for a picture of precision

TanDEM-X Earth Observation Satellite TanDEM-X (‘TerraSAR-X add-on for Digital Elevation Measurement’) is an Earth observation satellite, which, together with the almost identical TerraSAR-X radar satellite, forms a high-precision radar interferometer system.

The TerraSAR-X/TanDEM-X satellite formation can generate images similar to stereoscopic pictures. It is measuring all the Earth’s land surface (150 million square kilometres) within a period of less than three years. For a 12m grid (street width), surface height information can then be determined with an accuracy of under two meters. One goal is the production of a global Digital Elevation Model of unprecedented accuracy.

As for TerraSAR-X, the TanDEM-X project is a Public–Private Partnership between Astrium GmbH and the German space agency DLR. TanDEM-X was launched on 21 June 2010 from the Baikonur Cosmodrome (Kazakhstan) on board a Dnepr launcher and is designed for five years of operation.

Use of the data for scientific applications will be the responsibility of the DLR, commercial marketing of the data is managed by Astrium Services’ GEO-Information Division.

 

The Astrium  radar satellite TanDEM-X

The TanDEM-X mission will create a global Digital Elevation Model (DEM) with unprecedented accuracy.

© Astrium / Thomas Ernsting / 2010

 

Fact Sheet

 Customer DLR (Deutsches Zentrum für Luft- und Raumfahrt)
 Mission To generate a global Digital Elevation Model (DEM) with unprecedented accuracy
 Orbit Sun-synchronous dusk-dawn orbit
 Spacecraft Rebuild of the TerraSAR-X satellite which was based on the Astrium Flexbus concept and extensive heritage from the CHAMP and GRACE missions
 Payload

• Active phased array X-band Synthetic Aperture Radar (SAR)

• Tracking, Occultation and Ranging (TOR) equipment

 Features

• X-band downlink horn antenna is mounted at the tip of a 3.3m long boom
• Solid state mass memory capacity is 768Gbit
• High-pressure nitrogen gas propulsion system for formation flying

 Launch Mass 1340kg (spacecraft: 1220kg, fuel: 120kg)
 Dimensions 5m length, 2.4m diameter (hexagonal cross section)
 Launch Date June 2010 on DNEPR-1 rocket from Baikonur
 Mission Duration 5 years
 Astrium Responsibilities Prime contractor, SAR and satellite integration and testing, manufacturer of many electronic units including On-Board Computer and Solid State Mass Memory

 

Download the fact sheet (PDF)

Read the article by the BBC's science correspondent.

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