Luft- og romfartsteknikk

This document defines the primary space debris mitigation requirements applicable to all elements of systems launched into, or passing through, near-Earth space, including launch vehicle orbital stages, operating spacecraft and any objects released as part of normal operations or disposal actions. The requirements contained in this document are intended to reduce the growth of space debris by ensuring that spacecraft and launch vehicle orbital stages are designed, operated and disposed of in a manner that prevents them from generating debris throughout their orbital lifetime. This document is the top-level standard in a family of standards addressing debris mitigation. It will be the main interface for the user, bridging between the primary debris mitigation requirements and the lower-level implementation standards that will ensure compliance. This document does not cover launch phase safety for which specific rules are defined elsewhere. This document identifies the clauses and requirements modified with respect to ISO 24113, Space systems - Space debris mitigation requirements, Second edition 2011-05-15 for application in ECSS.

This document specifies the dimensions, tolerances and masses of rivets with 100° normal flush head, close tolerance, inch series, for aerospace application.

This document specifies the dimensions, tolerances and mass of rivets with universal head, close tolerance, inch series, for aerospace application.

This document specifies the dimensions, tolerances and mass of rivets with 100° reduced flush head, close tolerance, inch series, for aerospace application.

This document specifies the dimensions, tolerances and mass of rivets with 100° medium flush head, close tolerance, inch series, for aerospace application.

This document specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, operation and maintenance of aircraft movement equipment when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some performance requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies. This document applies to: - aircraft tractors with driver accommodation; - pedestrian controlled aircraft movement equipment; - moveable parts of ramp integrated systems; - attachment bars, used for all operations, utilizing aircraft movement equipment, e.g.: - push back; - maintenance towing. Designers of towbarless tractors will in addition take into account the requirements of ISO 20683-1 or ISO 20683-2 as applicable (see Bibliography). This document does not apply to: - ground power installations on aircraft tractors; - fixed ramp integrated systems; - special towing equipment (e.g. for recovery); - dispatch towing tractors. This document deals with vibrations and noise which are considered as significant. Vibration measurements are dealt with in EN 1915-3. Noise measurements and reduction are dealt with in EN 1915-4. This document does not deal with hazards in respect to a standard automotive chassis and from other vehicles on the apron. This Part of EN 12312 is not applicable to aircraft movement equipment manufactured before the date of its publication. This part of EN 12312 is intended to be used in conjunction with EN 1915-1, EN 1915-2, EN 1915-3 (for vehicles) and EN 1915-4. This part of EN 12312 when used in conjunction with EN 1915-1, EN 1915-2, EN 1915-3 and EN 1915-4 provides the requirements for GSE.