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The animation above is
a computer model of the objects being tracked by USSPACECOM radar, including large
pieces of orbital debris. White dots represent active payloads, while red dots represent defunct spacecraft, and other junk.
Click here to see to the Quicktime movie version of this animation.
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The environment of space above the earth is cluttered with millions of naturally
occurring micrometeoroids and man-made orbital debris. The past 40 years of
space exploration has unfortunately generated a lot of junk that threatens the
reliabiity of spacecraft. Orbital debris includes things as large spent rocket
stages and old satellites, to objects as small as flakes of paint and small metal
fragments. Even these tiny particles can seriously damage a spacecraft, because they
are traveling at very high speeds. In low earth orbit (LEO) man-made debris travels
around the Earth at speeds of roughly 7.5 kilometers per second.
That's almost 17,000 miles per hour! If two objects in orbit were to collide head-on,
the impact velocity would be double: 15 km/s or 34,000 mph. In general, micrometeoroids are in
orbit around the sun and can reach velocities in excess of 70 km/s, but they are usually
much smaller and less dense than orbital debris.
The orbital debris environment is growing. More and more satellites are launched
every year, and this adds to the orbital debris population. Obsolete satellites
can explode or fragment, generating thousands of new and smaller debris particles.
NASA is working with other space faring nations to reduce the production of orbital
debris fragments. This activity is called debris mitigation.
The animation above is
a computer model of the objects being tracked by USSPACECOM radar, including large
pieces of orbital debris. The smallest object which is tracked by USSPACECOM is
roughly 20 cm in diameter. These objects can be avoided by maneuvering a spacecraft
out of the way. Smaller particles cannot be tracked, however, and encounters with
these debris comprise the greatest risk associated with spaceflight in the LEO
environment. NASA has developed an engineering model
of the meteoroid and orbital
debris environment. This model may be used to determine the expected particle flux
for given mission parameters. Spacecraft must be designed to withstand hypervelocity
impacts by these small, untrackable particles. Testing is required to investigate
hypervelocity impact phenomena, and to develop effective shielding. Current NASA Orbital debris
program activities are documented in the Orbital Debris Newsletter.
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