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Space Safety » Archive » Space Debris » Debris Remediation

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Inside Debris Remediation

  • Figure 7. EFT-1 postflight MMOD inspection results, crew module and hatch windows(left); Figure 8. Typical crew module window impact of ROI #19 (+Y forward). Internal fracture dimensions = 0.51 x 0.41 mm diameter, crater dimensions = 0.36 x 0.18 mm diameter, depth = 0.03 mmOrion EFT-1 Postflight MMOD Inspection
  • CubeSats launched from the International Space Station's Kibo module on October 4, 2012 (Credits: NASA).Small Satellites and Space Junk
  • D-Orbit Tests Core Technology in Space
  • How Pop-Music Helps in Space Debris Detection
  • Active Debris Removal: A Necessary Evil
  • How to De-Orbit a CubeSat
  • D-Orbit Add-on Deorbits Satellites without Sacrificing Fuel
  • Satellite Collision From Space Debris in Orbit (Edt)DebriSat: Creating Orbital Debris on Earth
  • ESA Discusses Active Debris Removal
  • Synchronized Tumbling: Developing a Space Debris Removal Skill
  • Sweeping Away Space Debris With Dust
  • Air Bursts Present a New Option to Handle Space Debris
  • ViviSat Mission Extension Vehicle
  • Missed Opportunity Shines Light on Satellite Repurposing
  • Sophisticated Rescue Saves AEHF-1 Satellite
  • ElectroDynamic Debris Eliminator Receives Funding
  • Swiss Open Political Door for Space Debris Removal
  • DARPA Phoenix Program to Recycle Space Debris
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