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ISO 19683:2017
Space systems — Design qualification and acceptance tests of small spacecraft and units
Translate name
STANDARD published on 14.8.2017
The information about the standard:
Designation standards: ISO 19683:2017
Publication date standards: 14.8.2017
SKU: NS-693608
The number of pages: 85
Approximate weight : 286 g (0.63 lbs)
Country: International technical standard
Category: Technical standards ISO
The category - similar standards:
Annotation of standard text ISO 19683:2017 :
Description / Abstract: ISO 19683:2017 provides test methods and test requirements for design qualification and/or acceptance of small spacecraft or units. It provides the minimum test requirements and test methods to qualify the design and manufacturing methods of commercial small spacecraft and their units and to accept the final products. ISO 19683:2017 places emphasis on achieving reliability against infant mortality after satellite launch to orbit while maintaining low cost and fast delivery. ISO 19683:2017 is applied to satellites whose development methods are different from the ones used for traditional satellites that have little room for risk tolerance, as shown in Figure 1. The scope of this document encompasses different categories of small spacecraft, so-called mini-, micro, nano-, pico- and femto-, as well as CubeSat, spacecraft. Therefore, for the sake of convenience, the term "small spacecraft" is used throughout this document as a generic term. ISO 19683:2017 includes CubeSat, as long as it is developed with the untraditional processes.
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