V04 基础标准与通用方法 标准查询与下载
共找到 3175 条与 基础标准与通用方法 相关的标准，共 212 页
This Standard specifies requirements for mechanical testing of metallic materials to be used in the fabrication of spacecraft hardware. This Standard establishes the requirements for most relevant test methods carried out to assess the tensile, fatigue and fracture properties of metallic materials. It does not give a complete review of all the existing test methods for the evaluation of mechanical properties of metallic materials. Furthermore, this Standard specifies requirements for the evaluation, presentation and reporting of test results. This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.
Space product assurance - Mechanical testing of metallic materials
- ICS
- 49.025.01;49.140
- CCS
- V04
- 发布
- 2014-10
- 实施
Materials used in space applications need to be evaluated for their behaviour under Particle and UV Radiation. As part of this evaluation often an exposure to a simulated space environment is performed that can raise questions regarding its accuracy and representativeness. The role of this Standard is to establish a baseline for the testing specification. NOTE The environments covered are electromagnetic radiation and charged particles. This Standard defines the procedures for electromagnetic radiation and charged particles testing of spacecraft materials. These materials include for instance thermal control materials, windows, coatings, and structural materials. The procedures include simulation of the environment and the properties to be verified. This Standard excludes electronic components. This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.
Space product assurance - Particle and UV radiation testing for space materials
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-10
- 实施
Space environment (natural and artificial). Method of the solar energetic protons fluences and peak fluxes determination
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-09-30
- 实施
- 2014-09-30
Space engineering. Modal survey assessment
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-09-30
- 实施
- 2014-09-30
Space product assurance. ASIC and FPGA development
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-09-30
- 实施
- 2014-09-30
Space product assurance. Generic procurement requirements for hybrids
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-09-30
- 实施
- 2014-09-30
Space product assurance. Availability analysis
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-09-30
- 实施
- 2014-09-30
Space product assurance. Derating. EEE components
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-09-30
- 实施
- 2014-09-30
Space project management. Configuration and information management
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-09-30
- 实施
- 2014-09-30
Space product assurance. Critical-item control
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-09-30
- 实施
- 2014-09-30
Space product assurance. Failure modes, effects (and criticality) analysis (FMEA/FMECA)
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-09-30
- 实施
- 2014-09-30
Space product assurance. Nonconformance control system
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-09-30
- 实施
- 2014-09-30
Space product assurance. Off-the-shelf items utilization in space systems
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-09-30
- 实施
- 2014-09-30
Space engineering - Compatibility testing for liquid propulsion components@ subsystems and systems
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-09
- 实施
This clause contains the detailed specification of the logic of the Communications Operation Procedure-1 (COP-1) in the transfer sublayer. COP-1 consists of a pair of synchronized procedures which execute within one virtual channel at the sending and receiving ends of the transfer sublayer. At the sending end, the Frame Operation Procedure-1 (FOP-1) is executed. At the receiving end, a corresponding Frame Acceptance and Reporting Mechanism-1 (FARM-1) is executed. COP-1 is just one of the procedures performed within the transfer sublayer. It is the first procedure performed when a frame data unit (FDU) is received by the transfer sublayer at the sending end and the last one performed before the FDU is delivered to the next higher sublayer at the receiving end.
Space engineering - Space data links - Telecommand protocols@ synchronization and channel coding
- ICS
- 33.040.40;49.090;49.140
- CCS
- V04
- 发布
- 2014-09
- 实施
Space product assurance - Critical-item control
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-09
- 实施
Space engineering - Ranging and Doppler tracking
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-09
- 实施
Space product assurance - Quality assurance
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-09
- 实施
Space engineering - Solid propulsion for spacecrafts and launchers
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-09
- 实施
Space product assurance - Fault tree analysis - Adoption notice ECSS/IEC 61025
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-09
- 实施
