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
Space engineering - Structural design and verification of pressurized hardware; English version EN 16603-32-02:2014
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-10
- 实施
Space engineering - Structural finite element models; English version EN 16603-32-03:2014
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-10
- 实施
This Standard specifies requirements for preparing and assembling parts to be joined by wire wrapping, as well as the selection, calibration, use and certification of wire wrapping tools. The covered wire-wrapped connections are illustrated in Figure 1 1. This type of connection is similar to "Class A preferred" or "modified" connection detailed in MIL STD 1130, and NASA NHB 5300.4(3H). Only previously tested and qualified wire-wrapped connections are covered by this Standard, which includes four wire sizes from 24 AWG to 30 AWG, and three terminal post sizes up to 1,78 mm maximum diagonal. A step-by step procedure is covered in the informative Annex A. The use of heavier gauge wire and larger terminals is not generally prohibited, but it is considered unlikely that for such dimensions the method of wire-wrapping would be chosen as the electrical interconnection technique. Instead it is assumed that wire larger than 24 AWG will be multi-stranded and terminated by soldering in conformance with ECSS-Q-ST-70-08, or by crimping in conformance with ECSS-Q-ST-70-26. Training and certification requirements for operators and inspectors are defined in clause 5.6.7 and in ECSS-Q-ST-20. With effect from the date of approval, this Standard announces the adoption of the external document on a restricted basis for use in the European Cooperation for Space Standardization (ECSS) system. This standard may be tailored for the specific characteristic and constraints of a space project in conformance with ECSS-S-ST-00.
Space product assurance - Wire wrapping of high-reliability electrical connections
- ICS
- 49.140
- CCS
- V04
- 发布
- 2014-10
- 实施
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
