Customer Support: +44 (0)203 327 3140

Login to i2i Subscription Intertek.com
  • There are no items in your cart
We noticed you’re not on the correct regional site. Switch to our AMERICAS site for the best experience.
Go to AMERICAS site
Dismiss alert
Please enter a keyword to search
Advanced search
Home
BSI
BS ISO 16126:2014

BS ISO 16126:2014

Current

Current

The latest, up-to-date edition.

Space systems. Assessment of survivability of unmanned spacecraft against space debris and meteoroid impacts to ensure successful post-mission disposal

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

30-04-2014

Publisher

British Standards Institution

Foreword
1 Scope
2 Normative references
3 Terms and definitions
4 Abbreviated terms
5 Impact survivability assessment requirements
6 Impact survivability assessment procedure
7 Procedure for performing a simple impact
  risk analysis
8 Procedure for performing a detailed impact
  risk analysis
Annex A (informative) - Supplementary information
        on the simple impact risk analysis procedure
Annex B (informative) - Ballistic limit equations
Annex C (informative) - Background information
        on hypervelocity impact testing and modelling
Annex D (informative) - Method to calculate
        impact-induced Probability of No Failure
Annex E (informative) - Options for improving
        impact survivability
Bibliography

Specifies requirements and a procedure for assessing the survivability of an unmanned spacecraft against space debris and meteoroid impacts to ensure the survival of critical components required to perform post-mission disposal.

This International Standard defines requirements and a procedure for assessing the survivability of an unmanned spacecraft against space debris and meteoroid impacts to ensure the survival of critical components required to perform post-mission disposal. This International Standard also describes two impact risk analysis procedures that can be used to satisfy the requirements. The procedures are consistent with those defined in References [1] and [2].

This International Standard is part of a set of International Standards that collectively aim to reduce the growth of space debris by ensuring that spacecraft are designed, operated, and disposed of in a manner that prevents them from generating debris throughout their orbital lifetime. All of the primary debris mitigation requirements are contained in a top-level International Standard.[3] The remaining International Standards, of which this is one, provide methods and processes to enable compliance with the primary requirements.

Committee
ACE/68
DevelopmentNote
Supersedes 12/30213833 DC. (04/2014)
DocumentType
Standard
Pages
28
PublisherName
British Standards Institution
Status
Current
Supersedes

Standards Relationship
ISO 16126:2014 Identical

ISO 14200:2012 Space environment (natural and artificial) Guide to process-based implementation of meteoroid and debris environmental models (orbital altitudes below GEO + 2 000 km)
ISO 10795:2011 Space systems Programme management and quality Vocabulary
ISO 24113:2011 Space systems Space debris mitigation requirements
NSS 1740.14 : 0 ORBITAL DEBRIS MANUAL

View more information
£198.00
Excluding VAT
GBP
CAD
CHF
CNY
DKK
EUR
GBP
HKD
IDR
INR
JPY
KRW
MXN
NOK
NZD
SEK
SGD
USD
ZAR
Hardcopy - English
PDF - English
01
02
03
04
05
06
07
08
09
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50

Access your standards online with a subscription

Features

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.

Learn more on subscription solutions

or

Get in touch with us