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Hypervelocity impacts
Collision & re-entry risk control
 
ESA space debris studies: hypervelocity impact sample
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This image shows the results of a lab test impact between a small sphere of aluminum travelling at approximately 6.8 km/second 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: 1.2cm
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 6000 K.

Credits: European Space Agency, ESA

 
 
Hypervelocity impact testing
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EMI test 3915, 4.0 mm aluminium sphere, 7.2 km/s, 45 degrees 1.2 mm Al7075 bumper 49.5 mm spacing 3.3 Al7075 backwall

Credits: European Space Agency, ESA
 
  Whipple shielding
 
Whipple shield on ESA's Giotto comet investigator
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By spacecraft standards, the 960-kg Giotto was quite modest in size. Its main body was a short cylinder, 1.85m in diameter by about 1.1m in height. It contained three interior platforms: the top platform (30-cm thick), a main platform (40 cm), and an experiment platform (30 cm). Each of these consisted of a disc within the cylinder, on which were mounted various subsystems and science experiments. On top of the cylinder was a tripod which surrounded a 1.5-m diameter high-gain dish antenna, which gave the spacecraft a total height of 2.85m. The main rocket motor was positioned in the centre of the cylinder with the nozzle protruding from the bottom.

The most difficult problem to overcome was how to ensure that Giotto survived long enough to snap its close-up pictures of the comet nucleus when the spacecraft and the comet were heading towards each other at a combined speed of 245 000 km/hour (equivalent to crossing the Atlantic Ocean in 11 minutes!). At this speed, a 0.1-gram dust particle would be able to penetrate 8 cm of solid aluminium. Since it was out of the question to equip Giotto with a 600-kg aluminium shield, engineers turned to a more subtle, sandwich design first proposed by American astronomer Fred Whipple back in 1947 - long before the beginning of the Space Age.

The spacecraft's dust shield consisted of two protective sheets, 23cm apart. At the front was a sheet of aluminium (1-mm thick), which would vapourise all but the largest of the incoming dust particles. A 12-mm thick sheet of Kevlar at the rear would absorb any debris which pierced the front barrier. Together they could withstand impacts from particles up to 1 gram in mass and travelling 50 times faster than a bullet.

Credits: European Space Agency, ESA

 
 
Avoiding impacts: ESA's daily conjunction bulletin
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Daily conjunction bulletin send by ESA's collision avoidance system.

Credits: European Space Agency, ESA
 
 
First image Jules Verne ATV re-entry
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First images received from the DC-8 aircraft which observed the re-entry of Jules Verne ATV over the Pacific Ocean.

Credits: ESA
 
  Last update: 19 February 2009 


 
 
 
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