Luft- og romfartsteknikk

This document defines the requirements for hexavalent chromium free anodic electrodeposition of organic coatings on aluminium and aluminium alloys for corrosion protection of parts. The purpose of this document is to give design, quality and manufacturing requirements. It does not give complete in-house process instructions; these are given in the processors detailed process instructions.

This document specifies the requirements relating to: Steel X4CrNiMo16-5-1 (1.4418) Air melted Hardened and tempered Bars De ≤ 200 mm 900 MPa ≤ Rm ≤ 1 050 MPa for aerospace applications. NOTE Other common designations: AIR: Z 8 CND 17 04. Only the chemical composition of this document must be considered.

This document specifies the list of product standards and common characteristics of electrical cables for use in the on-board electrical systems of aircraft at operating temperatures between -55 °C and 260 °C (except otherwise specified in product document).

This document specifies the requirements relating to: Steel X4CrNiMo16-5-1 (1.4418) Air melted Hardened and tempered Forgings De ≤ 200 mm 900 MPa ≤ Rm ≤ 1 050 MPa for aerospace applications. NOTE Other common designations: AIR: Z 8 CND 17 04. Only the chemical composition of this document must be considered.

EN 16603-35-06 (equivalent of ECSS-E-ST-35-06) belongs to the Propulsion field of the mechanical discipline, and concerns itself with the cleanliness of propulsion components, sub-systems and systems The standard - defines design requirements which allow for cleaning of propulsion components sub-systems and systems and which avoid generation or unwanted collection of contamination, - identifies cleanliness requirements (e.g. which particle / impurity / wetness level can be tolerated), - defines requirements on cleaning to comply with the cleanliness level requirements, and the requirements on verification, - identifies the cleanliness approach, cleaning requirements, (e.g. what needs to be done to ensure the tolerable level is not exceeded, compatibility requirements), - identifies, specifies and defines the requirements regarding conditions under which cleaning or cleanliness verification takes place (e.g. compatibility, check after environmental test). The standard is applicable to

This standard addresses the requirements for performing verification by testing of space segment elements and space segment equipment on ground prior to launch. The document is applicable for tests performed on qualification models, flight models (tested at acceptance level) and protoflight models. The standard provides: • Requirements for test programme and test management, • Requirements for retesting, • Requirements for redundancy testing, • Requirements for environmental tests, • General requirements for functional and performance tests, NOTE Specific requirements for functional and performance tests are not part of this standard since they are defined in the specific project documentation. • Requirements for qualification, acceptance, and protoflight testing including qualification, acceptance, and protofight models’ test margins and duration, • Requirements for test factors, test condition, test tolerances, and test accuracies, • General requirements for development tests pertine

<p>This document defines detailed space debris mitigation requirements and recommendations for the design and operation of unmanned spacecraft in Earth orbit. The purpose of this document is to enable conformance with those high-level space debris mitigation requirements in <std std-id="iso:std:iso:24113:en" type="undated"><std-ref>ISO 24113</std-ref></std> that are relevant to spacecraft.</p><p>This document defines detailed requirements for the purpose of:</p><list list-type="alpha-lower"><list-item><label>a)</label><p>avoiding the intentional release of space debris into Earth orbit during normal operations;</p></list-item><list-item><label>b)</label><p>avoiding break-ups in Earth orbit;</p></list-item><list-item><label>c)</label><p>disposal of a spacecraft after the end of mission;</p></list-item><list-item><label>d)</label><p>estimating the mass of the remaining usable propellant;</p></list-item><list-item><label>e)</label><p>developing and maintaining the space debris mitigation plan.</p></list-item></list><non-normative-note><label>NOTE</label><p>This document does not cover nuclear power sources on spacecraft.</p></non-normative-note>

<p>This document deals with control systems developed as part of a space project. It is applicable to all the elements of a space control system, including the space segment, the ground segment and the launch service segment.</p><p>This document establishes general principles for all technical activities of space control engineering including control engineering management, requirements definition, analysis, design, production, verification and validation, operation, maintenance, and disposal. It also provides guidelines to progressively refine and manage control system realizations in space systems including multiple control systems.</p><p>The requirements of this international standard may be tailored for each specific space program application.</p>

<p>This document establishes requirements for the nomenclature, structure and contents of operational documents used at a launch pad or integration site.</p><p>When there is international participation, partnership or cooperation in the design, development, installation, test, activation or operation of a launch pad or integration site, this document applies to the development of the operational documents required for the following circumstances:</p><list list-type="dash"><list-item><label>—</label><p>installation, testing, activation or operation within the territory of one country of a launch pad or integration site manufactured in another country;</p></list-item><list-item><label>—</label><p>joint installation, testing, activation or operation when the equipment designed and manufactured in one country is part of the launch pad or integration site designed by another country;</p></list-item><list-item><label>—</label><p>training of the launch pad or integration site personnel of one country by the experts from another country.</p></list-item></list><p>The development and use of the operational documents described in this document are applicable to the following international launch pad or integration site operations:</p><list list-type="alpha-lower"><list-item><label>a)</label><p>preparation of integration site equipment to receive space vehicles and spacecraft;</p></list-item><list-item><label>b)</label><p>preparation of launch pad equipment and the space complex for the launch of space vehicles;</p></list-item><list-item><label>c)</label><p>space vehicle launch;</p></list-item><list-item><label>d)</label><p>post-launch maintenance of the integration site and launch pad;</p></list-item><list-item><label>e)</label><p>periodic maintenance of the integration site and launch pad.</p></list-item></list>