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  SEE PRODUCTS / SEE Related Model & DB - Meteoroid and Orbital Debris

ORDEM-2K

Description:

A semi-empirical, computer-based orbital-debris model has been developed which combines direct measurements of the environment with the output and theory of more complex orbital-debris models. It approximates the environment with six different inclination bands. Each band has a unique distribution of semi-major axis, for near circular orbits, and a unique perigee distribution, for highly elliptical orbits. In addition, each inclination band has unique size distributions which depend on the source of debris. Collision probability equations are used to relate the distributions of orbital elements to flux on a spacecraft or through the field of view of a ground sensor. The distributions of semi-major axis, perigee, and inclination are consistent with the U.S. Space Command catalogue for sizes larger than about 10 cm, taking the limitations of the sensors into account. For smaller sizes, these distributions are adjusted to be consistent with the flux measured by ground telescopes, the Haystack radar, and the Goldstone radar as well as the flux measured by the LDEF satellite and the Space Shuttle. The computer program requires less than one (1) second to calculate the flux and velocity distribution for a given size debris relative to an orbiting spacecraft.

Additional Information:

Language: binary executable

Operating System: Intel based computers only

Hardware Requirements: No special requirement

Availability:

  • Maintenance/ Upgrades: Unknown
  • Source Code: No
  • Cost: None
  • Distribution: 
  • Training: None

Input Description: Inputs are time in terms of calendar year, the solar activity in the year previous to the time, the limiting particle diameters, the altitude and the inclination of the spacecraft's orbit or the latitude of the fixed point.

Output Description: Flux, average velocity, velocity distribution, size, velocity, and angular distribution. All data are given in terms of cross-sectional data

Point of Contact:

Nicholas Johnson
NASA Johnson Space Center
Houston, Texas 77058

Phone: 281-483-5313
E-mail: nicholas.l.johnson1@jsc.nasa.gov

 
 


back to SEE Products - Meteoroid and Orbital Debris


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