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Hypervelocity particle capture: Some considerations regarding suitable target mediaHypervelocity particles colliding with passive capture media will be traversed by shock waves; depending on the stress amplitude, the particle may remain solid or it may melt or vaporize. Any capture mechanism considered for cosmic dust collection in low Earth-orbit must be designed such that sample alteration and hence loss of scientific information is minimized. Capture of pristine particles is fundamentally difficult, because the specific heat of melting and even vaporization is exceeded upon impact at typical, geocentric encounter velocities. From the results of calculated and observed melting behaviors it is concluded that shock stresses in excess of 50 GPA should be avoided during hypervelocity particle capture on board Space Station and that stresses 20 GPa, even at 15 km/s collision velocities, should constitute desirable instrument design goals. Some principal characteristics of the capture medium that may satisfy these requirements are identified.
Document ID
19860021120
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Horz, F.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Cintala, M. J.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
See, T. H.
(Lockheed Engineering and Management Services Co., Inc. Houston, Tex., United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Publication Information
Publication: Lunar and Planetary Inst. Trajectory Determinations and Collection of Micrometeoroids on the Space Station
Subject Category
Astrophysics
Accession Number
86N30592
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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