NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Orbital debris environment for spacecraft designed to operate in low Earth orbitThe orbital debris environment model is intended to be used by the spacecraft community for the design and operation of spacecraft in low Earth orbit. This environment, when combined with material-dependent impact tests and spacecraft failure analysis, is intended to be used to evaluate spacecraft vulnerability, reliability, and shielding requirements. The environment represents a compromise between existing data to measure the environment, modeling of this data to predict the future environment, the uncertainty in both measurements and modeling, and the need to describe the environment so that various options concerning spacecraft design and operations can be easily evaluated.
Document ID
19890013267
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kessler, Donald J.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Reynolds, Robert C.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Anz-Meador, Phillip D.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:100471
NASA-TM-100471
Report Number: NAS 1.15:100471
Report Number: NASA-TM-100471
Accession Number
89N22638
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available