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

Available format(s)

Hardcopy , PDF 1 User , PDF 3 Users , PDF 5 Users , PDF 9 Users

Language(s)

English

Published date

14-08-2017

Publisher

International Organization for Standardization

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.

DevelopmentNote	Supersedes ISO/DIS 19683. (08/2017)
DocumentType	Standard
Pages	85
ProductNote	This standard also referes to smc s 016, ecss-e-st-40c
PublisherName	International Organization for Standardization
Status	Current

Standards	Relationship
BS ISO 19683:2017	Identical

ISO 26869:2012	Space systems — Small-auxiliary-spacecraft (SASC)-to- launch- vehicle interface control document
NASA STD 7003 : 2011	PYROSHOCK TEST CRITERIA
MIL-STD-1540 Revision D:1999	TEST REQUIREMENTS FOR LAUNCH, UPPER-STAGE, AND SPACE VEHICLES
ISO 17770:2017	Space systems — Cube satellites (CubeSats)
ISO 24113:2011	Space systems Space debris mitigation requirements
ISO 11221:2011	Space systems Space solar panels Spacecraft charging induced electrostatic discharge test methods
MIL-STD-461 Revision G:2015	REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
ISO 15864:2004	Space systems General test methods for space craft, subsystems and units
ISO 14620-1:2002	Space systems Safety requirements Part 1: System safety
NASA STD 7001 : 2011	PAYLOAD VIBROACOUSTIC TEST CRITERIA
ISO 14302:2002	Space systems Electromagnetic compatibility requirements
ISO 17566:2011	Space systems General test documentation