Infoteenus
49 LENNUNDUS JA KOSMOSETEHNIKA
Uued standardid
EVS-EN 4165-018:2026
Aerospace series - Connectors, electrical, rectangular, modular - Operating temperature 175 °C continuous - Part 018: Protective cover for 1, 2 and 4 module receptacles series 2 and 3 - Product standard
Käsitlusala: This document specifies the protective cover for all receptacles series 2 and series 31 used in the family of rectangular electrical connectors.
The receptacle connectors corresponding to those protective covers are specified in EN 4165-004, EN 4165-011 and EN 4165-025.
The receptacle connectors corresponding to those protective covers are specified in EN 4165-004, EN 4165-011 and EN 4165-025.
Alusdokumendid: EN 4165-018:2026
Asendab: EVS-EN 4165-018:2015
EVS-EN 3545-005:2026
Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures - 55 C to 175 C - Part 005: Female coding and attachment System for mounting on free housing (plug) - Product standard
Käsitlusala: This document specifies the female coding and attachment system for mounting on free housing in the family of rectangular electrical connectors with sealed and non-sealed rear, plastic housing, locking device, for operating temperatures from -55 °C to 175 °C.
Alusdokumendid: EN 3545-005:2026
Asendab: EVS-EN 3545-005:2015
EVS-EN 6104:2026
Aerospace series - Rivets, solid, in aluminium or aluminium alloy - Inch series - Technical specification
Käsitlusala: This document specifies the characteristics and quality assurance requirements for solid rivets and slugs made in aluminium or aluminium alloys, inch series, for aerospace application. This document is applicable to the following aluminium alloys: 1050A-H14, 2017A-T42, 2117-T42, 5056A-H32 and 7050-T73.
Alusdokumendid: EN 6104:2026
ISO 1151-13:2026
Flight dynamics — Vocabulary — Part 13: Training devices
Käsitlusala: This document defines terms used in the field of pilot training with the use of technical equipment, called flight simulators, enhancing safety by allowing pilots to practice various scenarios in a controlled environments, without the need of an actual aircraft.
This document establishes the terms and definitions of the basic concepts applied in science, engineering and manufacturing in the field of flight simulation training devices (airplane and helicopter).
This document establishes the terms and definitions of the basic concepts applied in science, engineering and manufacturing in the field of flight simulation training devices (airplane and helicopter).
Alusdokumendid:
ISO 21384-3:2026
Uncrewed aircraft systems — Part 3: Operational procedures
Käsitlusala: This document specifies the requirements for safe commercial operations of uncrewed aircraft system (UAS), including the external safety-critical service providing command and control (C2) Link.
This document applies to all commercial UAS regardless of size, application or location and represents the international best practice for the safe commercial operation of any UAS.
This document applies to all commercial UAS regardless of size, application or location and represents the international best practice for the safe commercial operation of any UAS.
Alusdokumendid:
Asendab: ISO 21384-3:2023
ISO 14303:2026
Space systems — Launch-vehicle-to-spacecraft interfaces
Käsitlusala: This document specifies the interfaces between a launch vehicle (LV) and the spacecraft (SC) being launched, to provide LV and SC organizations with the necessary format for presenting the required technical data on existing and future interfaces.
Its intended purpose is to minimize costs and reduce the risks from errors resulting from miscommunication. It does not limit the ability of LV or SC organizations to specify unique requirements.
Its intended purpose is to minimize costs and reduce the risks from errors resulting from miscommunication. It does not limit the ability of LV or SC organizations to specify unique requirements.
Alusdokumendid:
Asendab: ISO 14303:2002
Asendatud standardid
EVS-EN 3545-005:2015
Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures -55 °C to 175 °C - Part 005: Female coding and attachment System for mounting on free housing (plug) - Product standard
Käsitlusala: This European Standard specifies the female coding and attachment system for mounting on free housing in the family of rectangular electrical connectors with sealed and non-sealed rear, plastic housing, locking device, for operating temperatures from –55 °C to 175 °C.
Alusdokumendid: EN 3545-005:2014
Asendatud: EVS-EN 3545-005:2026
EVS-EN 4165-018:2015
Aerospace series - Connectors, electrical, rectangular, modular - Operating temperature 175 °C continuous - Part 018: Protective cover for all receptacles series 2 - Product standard
Käsitlusala: This European Standard defines the protective cover for all receptacles series 2 used in the family of rectangular electrical connectors.
The connector accessory bodies corresponding to those protective covers are defined in EN 4165-004, EN 4165-011 and EN 4165-025.
The connector accessory bodies corresponding to those protective covers are defined in EN 4165-004, EN 4165-011 and EN 4165-025.
Alusdokumendid: EN 4165-018:2015
Asendatud: EVS-EN 4165-018:2026
ISO 14303:2002
Space systems -- Launch-vehicle-to-spacecraft interfaces
Käsitlusala: ISO 14303 specifies the interfaces between a launch vehicle (LV) and the spacecraft (SC) being launched, to provide LV and SC organizations with the necessary format for presenting the required technical data on existing and future interfaces. Its intended purpose is to minimize costs and reduce the risks from errors resulting from miscommunication. It does not limit the ability of LV or SC organizations to specify unique requirements.
Alusdokumendid:
Asendatud: ISO 14303:2026
ISO 15387:2005
Space systems -- Single-junction solar cells -- Measurements and calibration procedures
Käsitlusala: ISO 15387:2005 specifies the requirements for measurement and calibration procedures of single-junction space solar cells only. The main body of ISO 15387:2004 specifies the requirements for Air Mass Zero (AM0) standard calibration. The relative measurement procedures are provided as annexes.
Alusdokumendid:
ISO 21384-3:2023
Unmanned aircraft systems — Part 3: Operational procedures
Käsitlusala: This document specifies the requirements for safe commercial unmanned aircraft system (UAS) operations, including the external safety-critical service providing command and control (C2) link.
Alusdokumendid:
Asendatud: ISO 21384-3:2026
Kavandid
prEN 2328
Aerospace series - Washer, tab in corrosion resisting steel, cadmium plated for flight control rods - Dimensions
Käsitlusala: This document specifies the characteristics of tab washers for flight control rods.
These tab washers are intended to immobilise the rod end in relation to the rod body, whilst allowing a
positional adjustment of 1/2 a turn.
These tab washers are intended to immobilise the rod end in relation to the rod body, whilst allowing a
positional adjustment of 1/2 a turn.
Alusdokumendid: prEN 2328
prEN 9300-230
Aerospace series - LOTAR - LOng Term Archiving and Retrieval of digital technical product documentation such as 3D, CAD and PDM data - Part 230: As-built/As-delivered/As-maintained
Käsitlusala: This document specifies the “as-built” data used for demonstrating completion of the build process and conformity of the product to type design. This document defines the minimum set of information to be archived to serve as a complete representation of an organization’s as-built data.
Alusdokumendid: prEN 9300-230