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NASA/JSC orbital debris modelsThe orbital debris models developed within the framework of the NASA Johnson Space Center's (JSC's) orbital debris program, are categorized as environment definition and risk assessment models. The EVOLVE, CHAIN and the orbital debris engineering model 1996 (ORDEM96) computer programs determine the past, present and future orbital particulate environment, while the BUMPER and debris assessment software (DAS) computer programs provide a means for evaluating the risks of specific space missions. These models are presented. To support these models and to conduct specialized analyses, NASA/JSC employs a range of auxiliary models, including explosion and collision satellite breakup models, hypervelocity impact ballistic limit models, orbit propagation and decay models, space traffic models and solid rocket motor effluent models.
Document ID
19980005919
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Johnson, Nicholas
(NASA Johnson Space Center Houston, TX United States)
Christiansen, Eric
(NASA Johnson Space Center Houston, TX United States)
Reynolds, Robert
(Lockheed Martin Space Mission Systems and Services Houston, TX United States)
Matney, Mark
(Lockheed Martin Space Mission Systems and Services Houston, TX United States)
Zhang, Jing-Chang
(Lockheed Martin Space Mission Systems and Services Houston, TX United States)
Eichler, Peter
(Lockheed Martin Space Mission Systems and Services Houston, TX United States)
Jackson, Al
(Lockheed Martin Space Mission Systems and Services Houston, TX United States)
Date Acquired
August 17, 2013
Publication Date
May 1, 1997
Subject Category
Astronautics (General)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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