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This document defines several subsets of the syntax specified in ISO/IEC 21122-1 as profiles. It also defines lower bounds on the throughput in the decoded domain via levels and the encoded domain via sublevels that a conforming decoder implementation shall support. Furthermore, it defines a buffer model to ensure interoperability between implementations in the presence of a latency constraint.

 

This document applies to forgings and rolled or forged bars manufactured from the stainless steels given in Table 1 and delivered according to the specifications given in ISO 9327-1.

 

This document specifies the general technical delivery conditions for steel flat products (plate/sheet and strip) used principally for the construction of pressure equipment. The general technical delivery requirements of ISO 404 also apply to products supplied in accordance with this document.

 

This document specifies the technical delivery conditions for plates and strip for pressure equipment made of non-alloy and alloy steels as specified in Tables A.1 and B.1. The requirements and definitions of ISO 9328-1 also apply to this document.

 

This document specifies the technical delivery conditions for plates and strip for pressure equipment made of nickel-alloy steels as specified in Tables A.1 and B.1. The requirements and definitions of ISO 9328-1 also apply to this document. NOTE This document offers the possibility of specifying products in accordance with European design codes and ASME-type design codes.

 

1.1 This document specifies the technical delivery conditions for forgings and for rolled or forged bars for construction of pressure equipment manufactured from the following steels: — non-alloy and alloy ferritic or martensitic steels with specified room temperature properties and supplementary requirements for elevated temperature properties, — nickel steels with specified low temperature properties, — weldable fine grain steels with high proof strength, — stainless steels. NOTE The term forgings covers open die forgings including ring rolled products as well as closed die forgings. 1.2 In addition to the requirements of this document, the general technical delivery requirements in ISO 404 apply, unless otherwise indicated.

 

This document specifies the technical delivery requirements for Non-alloy and alloy (Mo, Cr and CrMo) steels with specified elevated temperature properties for pressure equipment,which comply with the chemical composition of steels given in Table 1. This document applies to forgings and rolled or forged bars in thicknesses up to 250 mm (partly up to 500 mm) manufactured from the steels listed in Table 1 and to be delivered according to the specifications given in ISO 9327-1.

 

This document applies to forgings and rolled or forged bars in thicknesses up to 50 mm manufactured from the steels which comply to the chemical composition of steels given in Table 1 and to be delivered according to the specifications given in ISO 9327-1.

 

This document applies to forgings and rolled or forged bars in thicknesses up to 250 mm manufactured from fine grain steels (see NOTE 1) which comply with the chemical composition of steels given in Table 1 and to be delivered according to the specifications given in ISO 9327-1. NOTE 1 Fine grain steels are here understood as steels with grain size 6 or finer according to the grain size charts in ISO 643.

 

This document specifies requirements for flat products for pressure purposes made of stainless steels, including austenitic creep-resisting steels, in thicknesses as specified in Tables 7 to 10. The requirements and definitions of ISO 9328-1 also apply to this document.

 

This International Standard establishes technical requirements and guidelines for the quality assurance of COTS EEE components, ensuring that performance, quality, schedule, cost and other critical requirements are met throughout the entire life cycle of space mission. The family includes electro-optical components. This standard does not cover specific test items for different types of components.

 

This standard specifies the purpose, principle, timing, indicators and process of design and verification for diagnosability and reconfigurability of spacecraft. This standard is applicable to evaluate and design of diagnosability and reconfigurability in the whole life cycle including mainly the stages of ground design and working in-orbit. The evaluation and design of diagnosability and reconfigurability in other stage can also be referred to the implementation. This standard focuses on the subsystem of spacecraft can be reconfigured after a fault occurs, such as attitude and orbit control subsystem, power subsystem and TT&C subsystem.

 

The document specifies DLT related requirements for establishing, improving, preserving, and assessing the privacy capability of a DLT system. The target audience of the document includes but is not limited to developers, providers, users and auditors of DLT system. It will be especially useful for the controllers and processors holding responsibility and accountability for privacy protected data processing.

 

The scope of JPEG Trust Part 2 is to elaborate on Trust Profiles and Trust Reports, which are built on the Trust Indicators specified in JPEG Trust Part 1. In addition, JPEG Trust Part 2 provides a catalogue of snippets that can be used either on their own or in combination for the purpose of constructing trust profiles, which can be used for assessing the trustworthiness of media assets in given usage scenarios.

 

This document specifies the requirements for the HSI 1000BASE-T1 communication channel used to connect machines, attachments and expansion kits within an HSI infrastructure. This document specifies general, mechanical, environmental and electrical requirements for: HSI communication channels; HSI cable assemblies; HSI cables; HSI connectors.

 

This document specifies the requirements for the HSI single communication channel coupling connector system used to connect machines, attachments and expansion kits within an HSI infrastructure. This document specifies: The HSI single communication channel coupling plug, break-away connector and expansion connector; Functional, stylistic, geometric, mounting, mechanical, material and electrical requirements; Conformance testing of the HSI single communication channel coupling connector system.

 

This document specifies requirements and test methods to ensure absolute sealing of compressed gaseous hydrogen piping for gaseous hydrogen fuel cell–powered unmanned aircraft systems (HFC UAS). It applies to all piping—from the hydrogen storage cylinder through to the fuel cell—such that no hydrogen leakage occurs under normal operation, transient conditions, or fault scenarios. Compliance with these requirements enables HFC UAS operators and regulatory authorities to demonstrate and certify the absence of any hydrogen gas leaks, thereby ensuring flight safety.

 

This document specifies the required performance of attachable hydrogen cylinders for HFC UAS with power pack hydrogen fuel cell systems. This document specifies the minimum safety, performance, and integrity requirements for attachable hydrogen cylinders, which are key components of hydrogen fuel cell powered unmanned aircraft systems (HFC UAS), to ensure safe flight and intended performance. It is applicable only to systems in which the hydrogen fuel cell power generation system is unitized as a power pack.

 

This document describes methods of specifying and evaluating the performances of electric vehicle charging robots. This document is not applicable to wireless charging systems for electric vehicles. This document is not intended for the verification or validation of safety requirements.

 

This document describes methods and requirements for proof of delivery replacing the physical signature, while being as secure and trustworthy as physical signatures. It applies to situations where the traditional, physical signature is required by the service to be provided and where this traditional physical signature is not required by regulation. It applies to parcels delivered to recipients by postal operators and Logistic Service Providers (LSP). This document aims to meet or exceed the level of confidence associated with traditional, physical signatures. The new proof of delivery process will ascertain that the item is delivered to an authorized recipient or receiver and also prove that the recipient accepted the delivery. This document includes only the delivery process (forward flow).