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NASA Policy and Considerations Related to Orbital Debris

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Title: NASA Policy and Considerations Related to Orbital Debris


1
  • NASA Policy and Considerations Related to Orbital
    Debris

Information provided by Nicholas Johnson at JSC,
and all information is available from public
resources
2
What is Orbital Debris?
  • Space debris encompasses both natural (meteoroid)
    and artificial (man-made) particles.
  • Meteoroids are in orbit about the Sun
  • Orbital debris are man-made and in orbit about
    the Earth

Non-operational Spacecraft
Fragmentation and Mission-related Debris
Derelict Launch Vehicle Stages
3


Orbital Debris Detectors and Damage Potential
Potential Shuttle Damage



4
International Academy of Astronautics
  • The IAA, established in 1960, is a professional
    organization of approximately 1200 individuals
    with demonstrated expertise in one or more fields
    of astronautics.
  • The IAA published its first position paper on
    space debris in 1995. This was updated in
    2000-2001.
  • The position paper includes a section on
    Implementation of Debris Control Methods
  • A new Position Paper on Space Debris Mitigation
    was released in 2005.
  • This position paper addresses space debris issues
    and recommended mitigation measures separately
    for spacecraft and launch vehicles.

5
Inter-Agency Space Debris Coordination Committee
(IADC)
  • Established in 1993
  • To exchange information on space debris research
    activities between member space agencies
  • To facilitate opportunities for cooperation in
    space debris research
  • To review progress of ongoing cooperative
    activities and
  • To identify debris mitigation options
  • 11 members include all leading space agencies in
    the world from China, France, Germany, India,
    Italy, Japan, Russia, Ukraine, United Kingdom,
    and the United States, as well as ESA.
  • NASA delegation includes personnel from DoD,
    State, and the FCC
  • Developed consensus international orbital debris
    mitigation guidelines in October 2002 presented
    to the United Nations in February 2003.

Website www.iadc-online.org
6
Orbital Debris at the United Nations
  • Since 1994 the subject of orbital debris has been
    on the agenda of the Scientific and Technical
    Subcommittee (STSC) of the United Nations
    Committee on the Peaceful Uses of Outer Space
    (COPUOS).
  • A multi-year work plan culminated in the 1999
    Technical Report on Space Debris
    (A/AC.105/720), summarizing the world
    state-of-knowledge concerning measurements and
    modeling of the environment as well as identified
    orbital debris mitigation measures.
  • The IADC Space Debris Mitigation Guidelines were
    reviewed and discussed at STSC in both 2003 and
    2004.
  • During 2005 and 2006 a special STSC Working Group
    prepared draft Space Debris Mitigation
    Guidelines of the STSC of the COPUOS.
  • Space Debris Mitigation Guidelines adopted by
    consensus of the STSC of COPUOS on 21 February
    2007.
  • Full COPUOS approval anticipated in June 2007

7
Other Considerations
  • Our debris tracking policy and decision process
    for doing avoidance maneuvers
  • NASA conducts conjunction assessments and, as
    necessary, collision avoidance maneuvers for the
    Space Shuttle, ISS, a number of LEO robotic
    spacecraft, and the TDRS constellation. 
  • The decision to conduct a collision avoidance
    maneuver is based upon either a discrete
    probability of collision (e.g., in excess of 1 in
    10,000) or on an established miss distance.  The
    geometry of the conjunction is also taken into
    account.
  • Size of debris we/Space Command are able to track
  • The U.S. Space Surveillance Network (SSN),
    managed by U.S. Strategic Command, maintains a
    Satellite Catalog which is nearly complete for
    objects larger than 10 cm in LEO and larger than
    1 m in GEO. 
  • At ISS altitudes, the SSN can track objects as
    small as 5 cm.
  • How often do we check for possible collisions
  • For human space flight operations, conjunction
    assessments are performed multiple times per day,
    normally looking three days into the future. 
  • For robotic spacecraft, the conjunction
    assessments are performed less frequently but for
    longer prediction periods. 
  • What and when do we share this information with
    our International Partners
  • Conjunction information for ISS is shared with
    our Russian colleagues since they would be
    involved in executing a collision avoidance
    maneuver. 
  • With only a very few exceptions, NASA is not
    involved in conjunction assessments for foreign
    spacecraft operators.

8
Other Considerations (Cont)
  • What we perceive as the real risks or
    probabilities of impact to our spacecraft
  • The level of collision risk to spacecraft varies
    greatly on their size and altitude. 
  • We can mitigate the risks from debris larger than
    5-10 cm by collision avoidance. 
  • We can mitigate the risks from debris smaller
    than 1 cm by shielding (in most cases). 
  • For debris in between, our only option is to
    curtail the growth of that debris population.
  • Chinese ASAT test
  • The Chinese ASAT test in January 2007 created the
    largest debris cloud known to date. 
  • Not only does the debris range through all of LEO
    (actually up to 4000 km), but also most of the
    debris will be very long-lived, many decades to a
    century or more. 
  • The SSN is now tracking more than 1600 debris a
    total of 1257 had been officially cataloged as of
    1 April. 
  • The risk to ISS from the Chinese debris spiked
    immediately after the test and has now dropped
    below normal background levels.
  • To date, no avoidance maneuvers have been
    required of the ISS due this ASAT test
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