V04 基础标准与通用方法 标准查询与下载
共找到 3178 条与 基础标准与通用方法 相关的标准，共 212 页
Die in dieser Norm festgelegten Anforderungen betreffen und gelten fur Kunden und Lieferanten auf allen Ebenen. Diese Norm darf auf die speziellen Merkmale und Vorgaben eines Raumfahrt-Projekts nach ECSS-S-ST-00 ausgelegt werden.
Space project management - Part 60: Cost and schedule management
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-08
- 实施
This Standard defines the structural design verification of metallic and non-metallic pressurized hardware which includes pressure vessels, pressurized structures, pressure components (such as valves, pumps, lines, fittings, and hoses), and special pressurized equipment (e.g. batteries, heat pipes, cryostats, sealed containers, hazardous fluids container). External supports and structural interfaces of pressurized hardware are not covered by this standard. Solid propellant motor cases are not covered by this standard. Objectives of the associated verification process are primarily to demonstrate the qualification of design and performance, as meeting all specified requirements, and to ensure that the flight hardware is free from workmanship defects and acceptable for flight. This Standard applies to all space products and in particular to launch vehicles, transfer vehicles, re-entry vehicles, spacecraft, space station, landing probes and rovers, sounding rockets, payloads and instruments. This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.
Space engineering - Structural design and verification of pressurized hardware
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-08
- 实施
The purpose of this Standard is to define the Factors Of Safety (FOS), Design Factor and additional factors to be used for the dimensioning and design verification of spaceflight hardware including qualification and acceptance tests. This standard is not self standing and is used in conjunction with the ECSS-E-ST-32, ECSS-E-ST-32-02 and ECSS-E-ST-33-01 documents. Following assumptions are made in the document: - that recognized methodologies are used for the determination of the limit loads, including their scatter, that are applied to the hardware and for the stress analyses; - that the structural and mechanical system design is amenable to engineering analyses by current state-of-the-art methods and is conforming to standard aerospace industry practices. Factors of safety are defined to cover chosen load level probability, assumed uncertainty in mechanical properties and manufacturing but not a lack of engineering effort. The choice of a factor of safety for a program is directly linked to the rationale retained for designing, dimensioning and testing within the program. Therefore, as the development logic and the associated reliability objectives are different for: - unmanned scientific or commercial satellite, - expendable launch vehicles, - man-rated spacecraft, and - any other unmanned space vehicle (e.g. transfer vehicle, planetary probe) specific values are presented for each of them. Factors of safety for re-usable launch vehicles and man-rated commercial spacecraft are not addressed in this document. For all of these space products, factors of safety are defined hereafter in the document whatever the adopted qualification logic: proto-flight or prototype model. For pressurized hardware, factors of safety for all loads except internal pressure loads are defined in this standard. Concerning the internal pressure, the factors of safety for pressurised hardware can be found in ECSS-E-ST-32-02. For loads combination refer to ECSS-E-ST-32-02. For mechanisms, specific factors of safety associated with yield and ultimate of metallic materials, cable rupture factors of safety, stops/shaft shoulders/recess yield factors of safety and limits for peak Hertzian contact stress are specified in ECSS-E-ST-33-01. Alternate approach The factors of safety specified hereafter are applied using a deterministic approach i.e. as generally applied in the Space Industry to achieve the structures standard reliability objectives. Structural safety based on a probabilistic analysis could be an alternate approach but it has to be demonstrated this process achieves the reliability objective specified to the structure. The procedure is approved by the customer. This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.
Space engineering - Structural factors of safety for spaceflight hardware
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-08
- 实施
Diese Norm liefert die Mittel zur Identifizierung und Strukturierung samtlicher Masnahmen (Aktivitaten) und Informationen, die bei einer Projektuberprufung (kurz "Projektreview") erforderlich sind. Sie legt die Ziele der Informationen und Masnahmen fest, die fur die Durchfuhrung des Prozesses erforderlich sind. Weiterhin gibt sie in Form einer Checkliste die Informationen und Masnahmen an, die fur die bei den ECSS-Normen zum Management genannten wichtigen Projektreviews erforderlich sind. Diese Norm darf auf die speziellen Merkmale und Vorgaben eines Raumfahrtprojektes nach ECSS-M-ST-00 ausgelegt werden.
Space project management - Part 10-01: Organization and conduct of reviews
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-08
- 实施
This software engineering Standard concerns the "product software", i.e. software that is part of a space system product tree and developed as part of a space project. This Standard is applicable, to the extent defined by the tailoring process, to all the elements of a space system, including the space segment, the launch service segment and the ground segment. This Standard covers all aspects of space software engineering including requirements definition, design, production, verification and validation, transfer, operations and maintenance. It defines the scope of the space software engineering processes and its interfaces with management and product assurance, which are addressed in the Management (-M) and Product assurance (-Q) branches of the ECSS System, and explains how they apply in the software engineering processes. This Standard reflects the specific methods used in space system developments, and the requirements for the software engineering processes in this context. Together with the requirements found in the other branches of the ECSS Standards, this Standard provides a coherent and complete framework for software engineering in a space project. This Standard is intended to help the customers to formulate their requirements and suppliers to prepare their responses and to implement the work. This Standard is not intended to replace textbook material on computer science or technology, and such material is avoided in this Standard. The readers and users of this Standard are assumed to possess general knowledge of computer science. The scope of this Standard is the software developed as part of a space project, i.e. "Space system product software". This Standard also applies to the development of non-deliverable software that affects the quality of the deliverable product. This Standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.
Space engineering - Part 40: Software
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-08
- 实施
Der Anwendungsbereich dieser Norm umfasst die Beschreibung der Prozesse und die Festlegung der Anforderungen an das Informations-/Dokumentationsmanagement sowie das Konfigurationsmanagement von Produkten innerhalb eines Raumfahrtprogramms oder -projektes. Die in dieser Norm festgelegten Anforderungen betreffen und gelten fur Lieferanten und Kunden auf allen Ebenen. Diese Norm darf auf die speziellen Merkmale und Vorgaben eines Raumfahrtprojekts nach ECSS-S-ST-00 ausgelegt werden.
Space project management - Teil 40: Configuration and information management
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-08
- 实施
ECSS-E-ST-32-03 (Space engineering - Structural finite element models) defines the requirements for finite element models used in structural analysis. This Standard specifies the requirements to be met by the finite element models, the checks to be performed and the criteria to be fulfilled, in order to demonstrate model quality. The Standard applies to structural finite element models of space products including: launch vehicles, transfer vehicles, re-entry vehicles, spacecraft, landing probes and rovers, sounding rockets, payloads and instruments, and structural parts of all subsystems. This standard may be tailored for the specific characteristics and constrains of a space project in conformance with ECSS-S-ST-00.
Space engineering - Structural finite element models
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-08
- 实施
This Standard specifies the basic requirements to be imposed on the performance and assessment of modal survey tests in space programmes. It defines the terminology for the activities involved and includes provisions for the requirement implementation. This Standard specifies the tasks to be performed when preparing, executing and evaluating a modal survey test, in order to ensure that the objectives of the test are satisfied and valid data is obtained to identify the dynamic characteristics of the test article. This standard may be tailored for the specific characteristics and constrains of a space project in conformance with ECSS-S-ST-00.
Space engineering - Modal survey assessment
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-08
- 实施
Diese Norm stellt einen Uberblick zum Zweck und zu den Positionen der Spezifizierung technischer Anforderungen bereit, legt die verschiedenen Arten der Anforderungen fest und definiert Anforderungen an die TS und ihre Anforderungen. Dieses Dokument gilt fur alle Arten von Raumfahrtsystemen, -projekten und -produkten. Diese Norm darf auf die speziellen Merkmale und Vorgaben eines Raumfahrtprojektes nach ECSS-S-ST-00 ausgelegt werden.
Space engineering - Part 10-06: Technical requirements specification
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-08
- 实施
This Standard addresses the discipline of environmental control and life support (ECLS) and the interfaces to other disciplines of engineering and to the domains of management and product assurance. It also introduces the structure and applicability of the associated Level 3 Standards. The environmental control and life support systems (ECLSS) covered in this Standard includes those aspects relating to the assurance of a safe and comfortable environment for human beings undertaking a space mission. When other forms of life are accommodated on board, the ECLSS also ensures the appropriate environmental conditions for those living organisms. This Standard applies to all ECLSS for: all manned space endeavours and manrated space products, and any other form of life to be maintained on board. This standard may be tailored for the specific characteristics and constrains of a space project in conformance with ECSS-S-ST-00.
Space engineering - Part 34: Environmental control and life support (ECLS)
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-08
- 实施
Space engineering. Method for the calculation of radiation received and its effects, and a policy for design margins
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-07-31
- 实施
- 2014-07-31
Space engineering. Reference coordinate system
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-07-31
- 实施
- 2014-07-31
Space engineering. Human factors engineering
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-07-31
- 实施
- 2014-07-31
Space engineering. Electromagnetic compatibility
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-07-31
- 实施
- 2014-07-31
Process management for avionics - Counterfeit prevention - Part 1: Avoiding the use of counterfeit, fraudulent and recycled electronic components
- ICS
- 03.100.50;31.020;49.060;49.090
- CCS
- V04
- 发布
- 2014-07-01
- 实施
Process management for avionics - Counterfeit prevention - Part 2: Managing electronic components from non-franchised sources
- ICS
- 03.100.50;31.020;49.090
- CCS
- V04
- 发布
- 2014-07-01
- 实施
Space engineering - Electromagnetic compatibility
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-07
- 实施
Space engineering - Reference coordinate system
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-07
- 实施
Space engineering - Human factors engineering
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-07
- 实施
