Norm

ISO/DIS 19683:2016 en

Space systems - Design qualification and acceptance tests of small spacecraft and units

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Over deze norm

Status Ontwerp
Aantal pagina's 78
Commissie Lucht- en ruimtevaart
Gepubliceerd op 24-08-2016
Taal Engels
This standard describes 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. This standard places emphasis on achieving reliability against infant mortality after satellite launch to orbit while maintaining low-cost and fast-delivery. A small spacecraft is a satellite that utilizes untraditional risk-taking development and management approaches to achieve low-cost and fast-delivery with a small number of team. The satellite size is small merely as a result of seeking low-cost and fast delivery. To achieve these two points, the satellite design relies on the use of non-space-qualified commercial-off-the-shelf (COTS) units and the satellite size inherently becomes smaller. The design accepts a certain level of risk associated with the use of COTS. This document is applied to satellites whose development methods are different from the ones used for traditional satellites that have little room of risk tolerance as shown in Fig.1. The scope of this standard 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. This standard includes CubeSat as long as it is developed with the untraditional processes.

Details

ICS-code 49.140
Nederlandse titel Space systems - Design qualification and acceptance tests of small spacecraft and units
Engelse titel Space systems - Design qualification and acceptance tests of small spacecraft and units

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