Space-Propulsion.com EADS Astrium
  Location: Home > Space Propulsion


Space Propulsion.com Home

Lampoldshausen Showcase.

Lampoldshausen
Showcase

AlphaBus
ARD
Ariane 5 ACS
Artemis
ATV
EuroStar
Galileo - NASA
Galileo - ESA
Mars Express
Meteosat
Rocsat
TerraSAR-X

VEGA - RACS






 


Automated Transfer Vehicle (ATV) Propulsion

Satellite and spacecraft propulsion systems from Astrium Lampoldshausen

 

The Automated Transfer Vehicle (ATV) is an unmanned spacecraft designed to transfer logistics and stores to the permanent crew of the International Space Station (ISS), 400 km above the Earth. It is the first European spacecraft to have a docking capability. The ATV will also be used to periodically restore the operational orbit of the Space Station.

The first ATV was named 'Jules Verne' and was launched by an ES ATV version of Ariane 5 on 9 March 2008.

The ATV will travel to the ISS about every 15 months, carrying up to 7.2 tonnes of equipment, spares, food, air and water from its Kourou launch site in French Guiana.

An on board high precision navigation system will guide the ATV on a rendezvous trajectory towards ISS, where it will automatically dock with the Station's Russian service module.

Once docked, the ATV will remain as a pressurised and integral part of the Station for up to six months. Before de-docking, the ATV will be loaded with up to 6.5 tonnes of waste material, ready for departure, de-orbitation and burn-up in the Earth's atmosphere.

 

 Automated Transfer Vehicle - Key Facts

Automated Transfer Vehicle during acoustic testing

Dimensions
Length
Largest diameter
Solar arrays span

Mass budget
Vehicle dry mass:
Vehicle consumables
Total vehicle mass
Total cargo upload capacity
Mass at launch
Waste download capacity

Launch Configuration
Cargo mass




Launch vehicle
Launch site
First flight


9.79 m
4.48 m
22.28 m

(420 km x 51.6 deg inclination)
10,470 kg
2,613 kg
13,083 kg
7,500 kg
20,750 kg
6,300 kg


Dry cargo: 1,500-5,500 kg
Water: 0-840 kg
Gas (N2, O2, air, 2 gasses/flight): 0-100 kg
ISS refuelling propellant: 0-830 kg
Total cargo upload capacity: 7,667 kg
Ariane 5 (300x300 km, 51.6° transfer orbit)
Kourou, French Guiana
2007

 

t


 

Automated Transfer Vehicle - Propulsion System
 

The ATV propulsion system comprises 4 x 490 N main engines and 28 x 200 N attitude control thrusters.

The Lampoldshausen centre is responsible for the production, integration and acceptance testing of the

ATV propulsion module pressure control assemblies (PCA)
Propellant Isolation Assembly (PIA)
Attitude control thruster clusters (ACS and FACS).

A pictorial insight into some of the ATV activities, performed at Astrium Lampoldshausen, is shown below:

Integration - Sub-Systems


ATV integrated thruster cluster.

Thruster Cluster

ATV Pressure Control Assembly

Pressure Control Assembly

 

 

Manufacturing of feed-line tubing system

CNC and manual tube bending, TIG orbit welding, visual inspection, X-ray
inspection, fluorescent dye penetrant inspection and cleanliness verification.

ATV feed system tubing.

Enlarge

 

 

Pre-Assembly on Welding Jig


 



Hot-Fire Testing


ATV bipropellant propulsion system under hot-fire testing at the Lampoldshausen  rocket engine test centre.

Enlarge

A video clip of ATV propulsion during
hot-fire testing is provided in the
Video Library

Propulsion Qualification Module (PQM)
integrated to the test stand at the
Lampoldshausen hot-fire test facility.

 

 

Contact for Further Information


If you require more detailed information on any of our products or services, then please contact us, indicating your particular areas of interest or intended application. Your enquiry will receive our best attention.

Copyright © 2003 - 2009 EADS Astrium | Google Search | Legal Notice and Imprint | Contact