M00027674
New product
SPACE SYSTEMS - TEST PROCEDURE TO EVALUATE SPACECRAFT MATERIAL EJECTA UPON HYPERVELOCITY IMPACT
International Organization for Standardization
In stock
Warning: Last items in stock!
Availability date: 11/05/2021
Foreword
Introduction
1 Scope
2 Normative references
3 Terms, definitions, abbreviated terms and symbols
4 General requirements
5 Calibration
6 Experimental procedure
7 Reporting of test results
8 Quality assurance
Annex A (informative) - Characterization of material ejected
upon impact (ejecta)
Annex B (informative) - Example of an ejecta model
Annex C (informative) - Ejecta measurement methods
Annex D (informative) - Example of a data sheet
Annex E (informative) - Technical data
Bibliography
Specifies an experimental procedure for assessing the behaviour, under orbital debris or meteoroid impacts, of materials that are intended to be used on the external surfaces of spacecraft and launch vehicle orbital stages.
Published | |
Document Type | Standard |
Status | Current |
Publisher | International Organization for Standardization |
Pages | |
ISBN | |
Committee | TC 20 |
Supersedes |
|