Space systems — Explosive systems and devices

This document specifies criteria and requirements for the use of explosive systems and explosive devices commonly used on spacecraft and other space products, including launch vehicles and space vehicle systems. It addresses the aspects of design, analysis, verification, manufacturing, operations and safety. To the greatest extent possible, requirements from past and existing standards have been analyzed, selected and tailored to be incorporated herein. In addition, the requirements herein include those generated as a result of lessons learned from launch and space vehicle programs. NOTE Specific requirements for man-rating are not addressed.

Systèmes spaciaux — Dispositifs et equipements explosifs

General Information

Status
Published
Publication Date
18-Oct-2020
Current Stage
6060 - International Standard published
Start Date
19-Oct-2020
Due Date
05-Jul-2020
Completion Date
19-Oct-2020
Ref Project

Relations

Standard
ISO 26871:2020 - Space systems -- Explosive systems and devices
English language
77 pages
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Standards Content (Sample)


INTERNATIONAL ISO
STANDARD 26871
Second edition
2020-10
Space systems — Explosive systems
and devices
Systèmes spaciaux — Dispositifs et equipements explosifs
Reference number
©
ISO 2020
© ISO 2020
All rights reserved. Unless otherwise specified, or required in the context of its implementation, no part of this publication may
be reproduced or utilized otherwise in any form or by any means, electronic or mechanical, including photocopying, or posting
on the internet or an intranet, without prior written permission. Permission can be requested from either ISO at the address
below or ISO’s member body in the country of the requester.
ISO copyright office
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Phone: +41 22 749 01 11
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Published in Switzerland
ii © ISO 2020 – All rights reserved

Contents Page
Foreword .v
Introduction .vi
1 Scope . 1
2 Normative references . 1
3 Terms, definitions, abbreviated terms and symbols . 1
3.1 Terms and definitions . 1
3.2 Abbreviated terms . 8
3.3 Symbols .10
4 Requirements .10
4.1 General .10
4.1.1 Background information .10
4.1.2 Overview .10
4.1.3 Applicability .11
4.1.4 Properties .11
4.2 Design .11
4.2.1 General.11
4.2.2 Debris requirements.12
4.2.3 Reliability and confidence levels .13
4.2.4 Performance .13
4.2.5 Wanted and unwanted response .13
4.2.6 Dimensioning .13
4.3 Mission .16
4.4 Functionality .16
4.5 Safety .17
4.5.1 General.17
4.5.2 Prevention of unintentional function .17
4.6 Survival and operational conditions .18
4.7 Interface requirements .19
4.7.1 General.19
4.7.2 Functional .19
4.7.3 Internal .19
4.7.4 External .20
4.8 Mechanical, electrical, and thermal requirements .20
4.8.1 Mechanical .20
4.8.2 Electrical .21
4.8.3 Thermal.24
4.8.4 Status check.25
4.9 Materials .26
4.10 Production lot .27
4.11 Non-explosive components and equipment .27
4.11.1 Connectors .27
4.11.2 Wiring .27
4.11.3 Shielding.28
4.11.4 Faraday cap .28
4.11.5 Safety cap.28
4.11.6 Power .28
4.11.7 Arm plug receptacle .29
4.11.8 Safe plug .29
4.11.9 Arm plug . .30
4.11.10 Test plug .30
4.11.11 Safe and arm device.30
4.11.12 Initiator harness connector .32
4.11.13 Initiator test substitute.32
4.12 Explosive components .32
4.12.1 General.32
4.12.2 Initiators, cartridges, detonators and packaged charges .33
4.12.3 Through-Bulkhead initiators .38
4.12.4 Integral initiator connectors .38
4.12.5 Transfer devices .39
4.12.6 Safe and arm devices containing explosive .40
4.12.7 Gas generators .41
4.12.8 Shaped charges.41
4.12.9 Expanding tube separation system .42
4.12.10 Distribution boxes .43
4.12.11 Explosive delays .44
4.13 Explosively actuated devices .45
4.13.1 General.45
4.13.2 Separation nuts and separation bolts .46
4.13.3 Pullers .47
4.13.4 Pushers (Thrusters) .48
4.13.5 Cutters .48
4.13.6 Pyro-valves .49
4.14 Items external to the flight equipment .50
4.14.1 GSE .
...

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