49.025.01 航空航天制造用材料综合 标准查询与下载

GB/Z 41275.22-2023 航空电子过程管理 含无铅焊料航空航天及国防电子系统 第22部分：技术指南

Process management for avionics—Aerospace and defence electronic systems containing lead-free solder—Part 22: Technical guidelines

GB/Z 41275.23-2023 航空电子过程管理 含无铅焊料航空航天及国防电子系统 第23部分：无铅及混装电子产品返工/修复指南

Avionics Process Management Aerospace and Defense Electronic Systems Containing Lead-Free Solder Part 23: Rework/Repair Guidelines for Lead-Free and Mixed Electronics

GB/Z 41275.4-2023 航空电子过程管理 含无铅焊料航空航天及国防电子系统 第4部分：球栅阵列植球

Avionics Process Management Aerospace and Defense Electronic Systems Containing Lead-Free Solder Part 4: Ball Grid Array Ball Installation

GB/T 42846-2023 空间环境 非金属材料空间辐射效应地面模拟方法

Ground simulation method for space radiation effect of non-metallic materials in space environment

GB/T 41886-2022 运输类飞机舱内声学设计要求

本文件规定了运输类飞机研制过程中舱内声学设计和验证的通用技术要求。 本文件适用于运输类飞机舱内声学设计与验证。其他机型开展舱内声学设计与验证,也可参照本文件的有关内容执行。

Requirements for cabin acoustic design of transport aircraft

GB/T 41275.21-2022 航空电子过程管理 含无铅焊料航空航天及国防电子系统 第21部分：向无铅电子过渡指南

本文件规定了在项目管理层或系统工程管理层对含无铅焊料航空航天及国防电子系统过渡的管理要求,以保证产品的性能和可靠性。 本文件适用于航空航天、国防电子系统行业,其他高性能、高可靠性行业可参照使用。

Process management for avionics—Aerospace and defence electronic systems containing lead-free solder—Part 21：Guidelines for transition to lead-free electronics

GB/T 41275.3-2022 航空电子过程管理 含无铅焊料航空航天及国防电子系统 第3部分：含无铅焊料和无铅管脚的系统性能试验方法

本文件规定了含无铅焊料和无铅管脚的系统性能的试验方法、试验规程和说明事项等内容。 本文件适用于航空航天及国防电子系统向无铅焊料过渡的产品,其他高性能、高可靠性电子行业可参考使用。 注:向无铅焊料过渡的产品包括:。 ———已通过传统铅锡电子元器件、材料和组装工艺的设计和鉴定,但正在使用无铅元器件进行重新鉴定的产品; ———采用锡铅设计转换为无铅焊料的产品; ———采用无铅焊料新设计的产品; ———组装焊接级产品,即印制板组装件级产品。

Process management for avionics—Aerospace and defence electronic systems containing lead-free solder—Part 3：Performance testing for systems containing lead-free solder and finishes

GB/T 41275.2-2022 航空电子过程管理 含无铅焊料航空航天及国防电子系统 第2部分：减少锡有害影响

本文件规定了在为减少电子系统无铅锡有害影响所采取缓解措施的过程中,对锡须的控制等级选择、各控制等级要求、实施方法、减少无铅锡影响的方法、零件选择过程、风险和缓解措施有效性评估和记录等技术要求。 本文件适用于航空航天、国防和高性能电子应用领域,其他高性能和高可靠性电子行业可参考使用。

Process management for avionics—Aerospace and defence electronic systems containing lead-free solder—Part 2：Mitigation of deleterious effects of tin

GB/T 41215-2021 空间材料科学实验 地面匹配试验规范

本文件规定了开展空间材料科学实验地面匹配试验的分类、目的和试验时机,内容与技术状态,要求,组织实施与分工,故障预案及处理方式和试验结果评估。 本文件适用于开展空间材料科学实验而进行的地面匹配试验。其他相关匹配试验可参照执行。1.1 主题内容1.2 适用范围

Space materials science experiment—Ground-based matching test specification

T/QGCML 3916-2024 飞行器用复合材料热压罐成型模具

本文件规定了飞行器用复合材料热压罐成型模具的术语和定义、产品结构、要求、试验方法、检验规则、标志、包装、运输和贮存。 本文件适用于飞行器用复合材料热压罐成型模具的生产和检验。

Composite material autoclave forming mold for aircraft

T/ZXJY 008-2023 间位芳纶纸蜂窝芯材

本文件规定了间位芳纶纸蜂窝芯材的术语和定义、芯材类别、规格和标记、原材料要求、技术要求、试验方法、检验规则、标识、包装、运输和贮存。

Meta aramid paper honeycomb core materials

T/CSCM 01-2023 民用航空发动机风扇包容机匣复合材料冲击侵彻抗性试验方法

本标准规定了一种使用特定夹持方式，通过发射钛合金弹片冲击聚合物基复合材料平板，从而获取其冲击侵彻抗性的测试方法，包括试验设备、试验条件、试件及冲击物、试验步骤、计算和试验报告等技术要求.

Test method for impact penetration resistance of composite materials for civil aviation engine fan containment casings

DB51/T 2973-2022 航电系统产品用芳纶纸蜂窝制件工艺质量控制要求

本文件规定了航电系统产品中使用的浸渍酚醛树脂芳纶纸制成的蜂窝芯材制件机械加工的工艺质量控制的一般要求。 本文件适用于航电系统产品中使用的纸蜂窝夹层板、吸波蜂窝芯材制件的机械加工工艺。

Process quality control requirements for aramid paper honeycomb parts used in avionics system products

DB51/T 2974-2022 航电系统产品用PMI泡沫制件工艺质量控制要求

本文件规定了航电系统产品用PMI泡沫的工艺与质量控制要求以及包装与贮存。 本文件适用于航电系统产品中的PMI泡沫制件。

Process quality control requirements for PMI foam parts used in avionics system products

T/ZZB 3027-2022 运载火箭用热振防护涂料体系

本文件规定了运载火箭用热振防护涂料体系的术语和定义、产品组成、基本要求、技术要求、 试验方法、 检验规则、标志、包装、运输和贮存及质量承诺。 本文件适用于由隔热涂料、烧蚀涂料、自辐射涂料组合的热流密度 500 kW/m2级的用于运载火箭箭体结构防热的烧蚀型防热涂料体系。

Thermal vibration protective coating system for launch vehicle

BS EN 3792:2022 航空航天系列 厌氧可聚合化合物 技术规格

1   Scope This document specifies the requirements for a range of one part anaerobic polymerisable compounds which polymerises upon the exclusion of oxygen and activation by a metal surface.

Aerospace series. Anaerobic polymerisable compounds. Technical specification

ASTM E1559-09(2022) 航天器材料污染排气特性的标准试验方法

1.1 This test method covers a technique for generating data to characterize the kinetics of the release of outgassing products from materials. This technique will determine both the total mass flux evolved by a material when exposed to a vacuum environment and the deposition of this flux on surfaces held at various specified temperatures. 1.2 This test method describes the test apparatus and related operating procedures for evaluating the total mass flux that is evolved from a material being subjected to temperatures that are between 298 and 398 K. Pressures external to the sample effusion cell are less than 7 × 10−3 Pa (5 × 10−5 torr). Deposition rates are measured during material outgassing tests. A test procedure for collecting data and a test method for processing and presenting the collected data are included. 1.3 This test method can be used to produce the data necessary to support mathematical models used for the prediction of molecular contaminant generation, migration, and deposition. 1.4 All types of organic, polymeric, and inorganic materials can be tested. These include polymer potting compounds, foams, elastomers, films, tapes, insulations, shrink tubing, adhesives, coatings, fabrics, tie cords, and lubricants. 1.5 There are two test methods in this standard. Test Method A uses standardized specimen and collector temperatures. Test Method B allows the flexibility of user-specified specimen and collector temperatures, material and test geometry, and userspecified QCMs. 1.6 The values stated in SI units are to be regarded as the standard. The values given in parentheses are for information only. 1.7 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.8 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

Standard Test Method for Contamination Outgassing Characteristics of Spacecraft Materials

OENORM EN 4258-2021 航空航天系列 金属材料 标准化总组织 欧洲标准类型及其使用之间的联系

Aerospace series - Metallic materials - General organization of standardization - Link between types of European Standards and their use

ASTM E1997-15(2021) 航天器材料选择的标准实施规程

1.1 The purpose of this practice is to aid engineers, designers, quality and reliability control engineers, materials specialists, and systems designers in the selection and control of materials and processes for spacecraft, external portion of manned systems, or man-tended systems. Spacecraft systems are very different from most other applications. Space environments are very different from terrestrial environments and can dramatically alter the performance and survivability of many materials. Reliability, long life, and inability to repair defective systems (or high cost and difficultly of repairs for manned applications) are characteristic of space applications. This practice also is intended to identify materials processes or applications that may result in degraded or unsatisfactory performance of systems, subsystems, or components. Examples of successful and unsuccessful materials selections and uses are given in the appendices. 1.2 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

Standard Practice for the Selection of Spacecraft Materials

BS EN 4866:2021 航空航天系列 有机基质复合材料中缺陷和缺陷的定义

Aerospace series. Definitions of imperfections and defects in organic matrix composite materials