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Micrometeoroid and orbital debris (MMOD) shield ballistic limit analysis program

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dc.contributor.author Ryan, Shannon
dc.contributor.author Christiansen, Eric L.
dc.date.accessioned 2019-08-23T16:58:35Z
dc.date.available 2019-08-23T16:58:35Z
dc.date.issued 2010-02
dc.identifier.uri https://hdl.handle.net/20.500.11753/1324
dc.description.abstract This software implements penetration limit equations for common micrometeoroid and orbital debris (MMOD) shield configurations, windows, and thermal protection systems. Allowable MMOD risk is formulated in terms of the probability of penetration (PNP) of the spacecraft pressure hull. en
dc.description.statementofresponsibility Shannon Ryan, Eric L. Christiansen
dc.description.tableofcontents Ballistic Limit Equations--Conclusions--Validation of Program Output
dc.format.extent viii, 76 pages
dc.format.mimetype application/pdf
dc.language.iso en en
dc.publisher Johnson Space Center en
dc.relation.ispartofseries LPI contribution ; no. 1804
dc.relation.ispartofseries MSC-24582-1
dc.relation.ispartofseries NASA technical memorandum ; 214789.
dc.subject Space vehicles--Meteoroid protection e
dc.subject Space debris en
dc.subject Ballistics en
dc.subject Space vehicles--Meteoroid protection en
dc.title Micrometeoroid and orbital debris (MMOD) shield ballistic limit analysis program en
dc.type Technical Report en


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    Documents the scientific research, meetings, and outreach products from the LPI.

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