NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
AbrasionParticle erosion of spacecraft surface is considered in aerospace vehicle and associated facility designs. When the speed of the spacecraft with relation to atmospheric suspended particles is high, erosion occurs even when the particles have a hardness less than the exposed surface. Surface impact damage parameters are developed for sand, dust, raindrops, snow, and hail particles at earth surface and at altitude.
Document ID
19740008185
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Daniels, G. E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 7, 2013
Publication Date
July 5, 1973
Publication Information
Publication: Terrest. Environ. (Climatic) Criteria Guidelines for Use in Aerospace Vehicle Develop., 1973 Rev.
Subject Category
Meteorology
Accession Number
74N16298
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available