ESAESOCSSASpacecraft OperationsGround Systems EngineeringSpace DebrisESOC History
   
OverviewESOC virtual tourMission historyFrequently asked questions
At ESOC
Mission operationsESTRACK tracking stations
Ground Systems Engineering
About Ground Systems EngineeringResearch and Technology DevelopmentEuropean software excellenceFlight DynamicsESA Navigation FacilityESA Space Debris OfficeGround Station Engineering
Activities
External servicesHSO ExchangeESA Ground Operation System (EGOS)
Multimedia
ESA Multimedia gallery
Media Centre
Press Releases
Services
PublicationsESA-sponsored ConferencesHelpPortal terms of useSubscribe
Visiting ESOC
Getting to ESOCGuided toursContact ESOC
 
 
 
Bookmark and Share
 
 
 
 
Article Images
Space debris: assessing the risk
 
16 March 2005

Hubble damage
Download:
 HI-RES JPG (Size: 413 KB)
Front view of penetration of Hubble Space Telescope (HST) solar array. Clear hole size: 2.5 mm. The HST solar array was retrieved in March 2002 after 8.25 years in space.

Credits: European Space Agency, ESA
 
  Deadly objects in 1- to 10-cm range
 
HVI
Download:
 HI-RES JPG (Size: 62.4 KB)
This image shows the results of a lab test impact between a small sphere of aluminum travelling at approximately 6.8 km per sec and a block of aluminum 18 cm thick. This test simulates what can happen when a small space debris object hits a spacecraft.

Al sphere diameter: 1.2-cm
Al sphere mass: about 1.7 g
Impact crater diameter: 9.0 cm
Impact crater depth: 5.3 cm

In such an impact, the pressure and temperature can exceed those found at the centre of the Earth e.g. greater than 365 GPa and more than 6,000 K.

Credits: European Space Agency, ESA

 


Related news
Debris is Shuttle's Biggest ThreatChina establishes 1st space trash observation center
Related links
Space debris spotlight (Part 1)6th Int. Symposium: Reducing Cost of Spacecraft Ground Systems & Operations (abstracts, PDF)European Centre for Space Law
 
 
 
   Copyright 2000 - 2012 © European Space Agency. All rights reserved.