This Standard specifies the physical interconnection media and data communication protocols to enable the reliable sending of data at highspeed (between 2 Mb/s and 400 Mb/s) from one unit to another. SpaceWire links are fullduplex, pointtopoint, serial data communication links. The scope of...
This Standard specifies the physical interconnection media and data communication protocols to enable the reliable sending of data at highspeed (between 2 Mb/s and 400 Mb/s) from one unit to another. SpaceWire links are fullduplex, pointtopoint, serial data communication links. The scope of...
This specification provides airworthiness design requirements for general aeroplane performance, and is applicable to small aeroplanes as defined in Terminology F3060. The applicant for a design approval shall seek the individual guidance to their respective civil aviation authority (CAA) body...
4.1 The term "electrical system" as used in this practice means those parts of the aircraft that generate, distribute, and use electrical energy, including their support and attachments. 4.2 The satisfactory performance of an aircraft is dependent upon the continued reliability of the electrical...
This specification provides airworthiness design requirements for general aeroplane performance, and is applicable to small aeroplanes as defined in Terminology F3060. The applicant for a design approval shall seek the individual guidance to their respective civil aviation authority (CAA) body...
This document describes SCCS architecture in terms of the following: - definitions of all key elements, on ground and in space, that are involved in space communications; - definitions of concepts that characterize SCCS services; - requirements on system elements and components that provide secure...
The present document is applicable to the Advanced Surface Movement Guidance and Control System (A-SMGCS) Routing Service. This service is based on the A-SMGCS surveillance service as specified in ETSI EN 303 213-1 [3] and generates individual routes for mobiles based on the...
4.1 The term "electrical system" as used in this practice means those parts of the aircraft that generate, distribute, and use electrical energy, including their support and attachments. 4.2 The satisfactory performance of an aircraft is dependent upon the continued reliability of the electrical...
The term "electrical system" as used in this practice means those parts of the aircraft that generate, distribute, and use electrical energy, including their support and attachments. The satisfactory performance of an aircraft is dependent upon the continued reliability of the electrical system....
The present document is applicable to the Advanced Surface Movement Guidance and Control System (A-SMGCS) Routing Service. This service is based on the A-SMGCS surveillance service as specified in ETSI EN 303 213-1 [3] and generates individual routes for mobiles based on the...
This specification covers minimum requirements for the design, manufacture, and installation of airframe emergency parachutes for light sport aircraft. Materials used for parts and assemblies, shall meet the conditions specified for (1) suitability and durability, (2) strength and other properties...
This specification covers minimum requirements for the design, manufacture, and installation of airframe emergency parachutes for light sport aircraft. Materials used for parts and assemblies, shall meet the conditions specified for (1) suitability and durability, (2) strength and other properties...
This specification covers minimum requirements for the design, manufacture, and installation of airframe emergency parachutes. Materials used for parts and assemblies, shall meet the conditions specified for (1) suitability and durability, (2) strength and other properties assumed in the design...
This specification covers minimum requirements for the design, manufacture, and installation of airframe emergency parachutes for light sport aircraft. Materials used for parts and assemblies, shall meet the conditions specified for (1) suitability and durability, (2) strength and other properties...
This specification covers minimum requirements for the design, manufacture, and installation of airframe emergency parachutes for light sport aircraft. Materials used for parts and assemblies, shall meet the conditions specified for (1) suitability and durability, (2) strength and other properties...
ESDU 08003 introduces the treatment of risk within the context of the performance of commercial air transport. The concept of risk is introduced in relation to what is considered safe by the aircraft operators, by the official bodies responsible for regulating air transport and implicitly by the...
This document specifies the requirements and recommendations for the design and test of RF components and equipment to achieve acceptable performance with respect to multipaction-free operation in service in space. The document includes: . verification planning requirements; . definition of a...
This standard defines the requirements and recommendations for the design and test of RF components and equipment to achieve acceptable performance with respect to multipactor-free operation in service in space. The standard includes: - verification planning requirements, - definition of a...