Luft- og romfartsteknikk

ISO 23460:2011 presents the requirements for a dependability (reliability, availability and maintainability) assurance programme for space projects.

ISO 23460:2011 defines the dependability requirements for space products as well as for system functions implemented in software, and the interaction between hardware and software.

The provisions of ISO 23460:2011 apply to all programme phases.

This Standard specifies the general requirements for the qualification, procurement, storage and delivery of photovoltaic assemblies, solar cell assemblies, bare solar cells, coverglasses and protection diodes suitable for space applications. This standard does not cover the particular qualification requirements for a specific mission. This Standard primarily applies to qualification approval for photovoltaic assemblies, solar cell assemblies, bare solar cells, coverglasses and protection diodes, and to the procurement of these items. This standard is limited to crystaline Silicon and single and multi-junction GaAs solar cells with a thickness of more than 50 m and does not include thin film solar cell technologies and poly-crystaline solar cells. This Standard does not cover the concentration technology, and especially the requirements related to the optical components of a concentrator (e.g. reflector and lens) and their verification (e.g. collimated light source). This Standard does not apply to qualification of the solar array subsystem, solar panels, structure and solar array mechanisms.

ISO 17689:2015 is applied for organizations developing ground support equipment and also for operators performing space activity.

Interface control documents format defined here does not contain the descriptions regarding various properties of ground support equipment (i.e. performance, functions or endurance to launch mechanical environment or quality assurance provisions) which are defined in technical specifications.

Control of interfaces, independently of its frequency or depth, cannot replace stages of parameters definition of high-quality production and development of technical requirements of project, design and development. Interfaces control is used as a control process that can provide necessary verification of successful finishing of design at a stated in contract period.

This International Standard establishes basic requirements for interface control documents (ICD) writing and interface control procedures for the following items included in launch system: payload, launch vehicle, ground support equipment (according to ISO 14625:2007) and launch site (buildings with technical systems). Notably

a) ICD between payload and launch vehicle (according to ISO 15863:2003),

b) ICD between ground support equipment and payload (this International Standard),

c) ICD between ground support equipment and launch vehicle (this International Standard),

d) ICD between items of ground support equipment (this International Standard), and

e) ICD between ground support equipment and launch site (this International Standard).

This document specifies minimum requirements for life rafts carried on helicopters operating in a hostile sea area or over very rough sea conditions. Life rafts covered by this document are for use by helicopter crew members and passengers in the event of a ditching or water impact. They are intended either for integration into the helicopter, or stowed in the cabin before being manhandled out of the helicopter. This document does not cover air-drop life rafts.

This document is applicable in the aeronautical domain to on-board parts and to equipment intended to be embedded or positioned on any civil or military airborne vehicle with a type certificate. The purpose of this document is to guide design, manufacturing, maintenance and operations organizations in the installation, removal and replacement of RFID tags (UHF and HF) and Contact Memory Buttons (CMB), according to the environments defined in RTCA DO-160/EUROCAE ED-14 and according to the type of support and the expected fixation performances. This guide will provide help in the specification of the tag installation/removal functions and/or will enable the solutions on offer from tag suppliers to be enhanced. The term "tag" used in this document covers all the tags used to store electronic data, including RFID tags and CMB tags. As a reminder, the tags can also contain information that can be read by devices other than RFID or CMB readers (e.g., bar codes - Data Matrix, QR codes, etc., and/or alphanumerical characters) and information that can be read by the naked eye without any tools (human-readable).

This document is applicable to new manufactured tags after publication of this document. This document aims to: - provide specification for RFID tag manufacturers to design and manufacture passive UHF RFID tags for the aeronautical industry; - identify required performances for UHF RFID tags in order to be read/written during ground operations only, while being subject to the global flight environment; - identify functional and environmental validation tests to be performed on passive UHF RFID tags with associated pass/fail criteria as well as associated test methods; - check functionalities and resistance to environment for airborne passive UHF RFID tags. This document does not cover: - the reader (interrogator - readers). It will be addressed appropriately by individual applicants; - active RFID devices or battery assisted passive (BAP) RFID devices; - RFID tags designed to operate outside the 860 to 960 MHz frequency range.