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
本标准规定了切割索与削弱槽对中度X射线照相检验的-般要求、技术准备、透照、暗室处理、评定、检验记录、检验报告及归档等要求。 本标准适用于航天弹体聚能切割索与削弱槽装配对中度的X射线照相检验。X射线数字成像检验可参照执行。
X-ray radiographic testing method for center coincidence departure between cutting charges and weakening groove of aerospace missile body
- ICS
- CCS
- V04
- 发布
- 2011-07-19
- 实施
- 2011-10-01
本标准规定了使用ADAMS软件进行机构动力学仿真分析的数据准备、分析流程、文档编写与管理等要求。 本标准适用于使用ADAMS软件进行机构动力学仿真分析及其文档的编写和管理。采用其它软件进行机构动力学仿真时可参照使用。
General requirements for dynamic analysis of mechanical system based on ADAMS
- ICS
- CCS
- V04
- 发布
- 2011-07-19
- 实施
- 2011-10-01
本标准规定了航天产品代号的编制方法和管理要求。 木标准适用于导弹、运载火箭、航天器的型号代号及其所属专用产通用产品的产品代号的编制和管理。
Drafting rules for space product codes
- ICS
- CCS
- V04
- 发布
- 2011-07-19
- 实施
- 2011-10-01
本标准为航天产品实施故障模式及影响分析（FMEA)与故障模式、影响及危害性分析（FMECA)提供指南。 本标准适用于航天产品研制过程中实施设计FMEA与FMECA、软件FMEA、工艺FMEA等工作。
Guide of failure modes effects and criticality analysis for space products
- ICS
- CCS
- V04
- 发布
- 2011-07-19
- 实施
- 2011-10-01
本标准规定了航天产品多余物预防和控制的管理要求，以及在设计、工艺、生产、试验、包装、运输等过程中的多余物预防和控制要求。 本标准适用于航天产品（软件产品除外）。其它产品可参照使用。
Prevention and control for foreign object debris (FOD) of space products
- ICS
- CCS
- V04
- 发布
- 2011-07-19
- 实施
- 2011-10-01
本标准规定了航天产品质量与可靠性信息的常用类别和信息项编码规则，给出了各类信息及信息单元的内容说明，列出了相关信息项内容及代码。 本标准适用于航天产品质量与可靠性信息分类与标识，便于信息的采集、存储、传递、处理和利用。
Classification and codes of quality and reliability information for space products
- ICS
- CCS
- V04
- 发布
- 2011-07-19
- 实施
- 2011-10-01
本标准规定了气相色谱-质谱检测法检测航天器表面沉积分子污染物成分的检测设备与采样用品、样品采样、检测准备、检测程序、检查结果定性分析、检测报告等。 本标准适用于航天器表面沉积分子污染物成分的检测分析。
Test method of contamination component for spacecraft
- ICS
- CCS
- V04
- 发布
- 2011-07-19
- 实施
- 2011-10-01
本部分规定了使用磁性测厚仪和涡流测量仪分别对磁性基体和非磁性基体金属上涂层厚度测量的一般要求、测量方法、检测数量及位置、测量的不确定度和报告。 本部分适用于航天产品有机涂料涂覆、热喷涂、釉瓷、搪瓷等涂层厚度的测量验收。其他产品涂层厚度的测量验收亦可参照执行。 本部分不适用于非金属基体上的涂层、小曲率半径的金属基体上的涂层等涂层厚度的测量验收。
Inspection methods of coating.Part 3:Measurement of coating thickness
- ICS
- CCS
- V04
- 发布
- 2011-07-19
- 实施
- 2011-10-01
This document provides a review of published methods that have been used to provideestimates of the levels of distortion and/or the concomitant loss of stability pressure ratio thatcan occur when the recommended full complement of aerodynamic interface plane highresponseinstrumentation is not used when obtaining inlet data. The methods have beencategorized based on the underlying mathematical representation of the aerophysics.Further, the use of maximum value statistics, which has been used to further improve theresults where short-duration time records have been employed, is discussed.
Distortion Synthesis/Estimation Techniques
- ICS
- CCS
- V04
- 发布
- 2011-07-01
- 实施
Space systems - Structural components and assemblies
- ICS
- 49.140
- CCS
- V04
- 发布
- 2011-07
- 实施
Dosimetry for exposures to cosmic radiation in civilian aircraft - Part 2: Characterization of instrument response
- ICS
- 17.240
- CCS
- V04
- 发布
- 2011-06
- 实施
Space projects. Programme management. Dependability assurance requirements
- ICS
- 49.140
- CCS
- V04
- 发布
- 2011-05-31
- 实施
- 2011-05-31
Space systems. Programme management. Project organization
- ICS
- 49.140
- CCS
- V04
- 发布
- 2011-05-31
- 实施
- 2011-05-31
This AIR documents the methodologies used to calculate the dimensions and tolerances used in the following backup rings standards: AS5781; AS5782; AS5860; AS5861. In addition, an appendix is provided with provides details of gland and backup ring design practices.
Calculations to Determine Dimensions for Backup Rings to AS5781, AS5782, AS5860, AS5861
- ICS
- 49.035;49.080
- CCS
- V04
- 发布
- 2011-05-25
- 实施
This Aerospace Information Report (AIR) is limited in scope to the general consideration of environmental control system noise and its effect on occupant comfort. Additional information onthe control of environmental control system noise may be found in the bibliography and in thedocuments referenced throughout the text. This document does not contain sufficient direction anddetail to accomplish effective and complete acoustic designs.
Acoustical Considerations for Aircraft Environmental Control System Design
- ICS
- CCS
- V04
- 发布
- 2011-01-01
- 实施
- 2011-01-01
This specification covers three types of deicing/anti-icing material, each in the form of a non-Newtonian fluid.
Fluid, Aircraft Deicing/Anti-Icing, Non-Newtonian (Pseudoplastic), SAE Types II, III, and IV
- ICS
- 49.025.99
- CCS
- V04
- 发布
- 2010-12-09
- 实施
This International Standard establishes general test requirements for launch vehicles equipped with liquid-propellant engines, launched from stationary ground-, sea- and air-based launchers, in all phases of their development.
Space systems - General test requirements for launch vehicles
- ICS
- 49.140
- CCS
- V04
- 发布
- 2010-10-15
- 实施
- 2010-10-15
Space systems - Probabilistic risk assessment (PRA)
- ICS
- 49.140
- CCS
- V04
- 发布
- 2010-08-31
- 实施
- 2010-08-31
本标准规定了航磁总场测量(简称航空磁测)的技术设计、仪器设备与检验、测量飞行与野外工作、数据处理与图件编制、异常查证、推断解释与成果报告编写等技术要求。 本标准适用于基础地质调查，能源、金属、非金属矿产地质勘查和水文、工程、环境地质勘查中的航空磁测工作，其他目的的航空磁测工作可参考使用。
Criterion of aeromagnetic survey
- ICS
- A77
- CCS
- V04
- 发布
- 2010-08-05
- 实施
- 2010-08-31
Space systems - Probabilistic risk assessment (PRA)
- ICS
- 49.140
- CCS
- V04
- 发布
- 2010-08
- 实施
