V70 航天器综合 标准查询与下载

BS EN 16603-32-03:2014 航天工程. 结构有限元模型

Space engineering. Structural finite element models

BS EN 16603-32:2014 航天工程. 通用结构要求

Space engineering. Structural general requirements

BS EN 16603-32-02:2014 航天工程. 加压硬件的结构设计和验证

Space engineering. Structural design and verification of pressurized hardware

BS EN 16603-32-10:2014 航天工程. 航天硬件的安全结构因素

Space engineering. Structural factors of safety for spaceflight hardware

ANSI/NFPA 1127-2013 大功率火箭规格

Code for High Power Rocketry

SAE ARP94910-2012 航空航天.车辆管理系统.军用无人机的飞行控制设计、安装和试验的规范指南

This document establishes recommended practices for the specification of general performance, design, test, development, and quality assurance requirements for the flight control related functions of the Vehicle Management Systems (VMS) of military Unmanned Aircraft (UA), the airborne element of Unmanned Aircraft Systems (UAS), as defined by ASTM F 2395-07. The document is written for military unmanned aircraft intended for use primarily in military operational areas. The document also provides a foundation for considerations applicable to safe flight in all classes of airspace.

Aerospace - Vehicle Management Systems - Flight Control Design, Installation and Test of, Military Unmanned Aircraft, Specification Guide for

ISO 26871:2012 空间系统.爆炸系统和设备

Space systems - Explosive systems and devices

ISO 14200:2012 空间环境(自然和人为).流星体和残骸环境模型基于流程实现的指南(轨道高度低于GEO + 2 000 km)

Space environment (natural and artificial) - Guide to process-based implementation of meteoroid and debris environmental models (orbital altitudes below GEO + 2 000 km)

BS ISO 11227:2012 航空系统.评估超高速撞击航空器材料喷出物的试验规程

Space systems. Test procedure to evaluate spacecraft material ejecta upon hypervelocity impact

BS ISO 22641:2012 航天数据和信息传送系统.TM(遥测技术)同步和信道编码

Space data and information transfer systems. TM (telemetry) synchronization and channel coding

BS ISO 15388:2012 空间系统.污染和清洁度控制

Space systems. Contamination and cleanliness control

ISO 15388:2012 空间系统.污染和清洁度控制

This International Standard establishes general requirements for contamination and cleanliness control that are applicable, at all tiers of supply, to the development of space systems, including ground processing facilities, ground support equipment, launch vehicles, spacecraft, payloads, and ground processing and on-orbit operations. It also provides guidelines for the establishment of a contamination and cleanliness control programme.

Space systems - Contamination and cleanliness control

BS ISO 10784-1:2011 航天系统.早期运行.宇宙飞船的初始化和调试

Space systems. Early operations. Spacecraft initialization and commissioning

ISO 10784-2:2011 航天系统.早期运行.第2部分:初始化计划

This part of ISO 10784 provides SC manufacturers and operators with a specific form and format to write spacecraft initialization plans required to configure and verify the SC to perform normal mission operations. Since the SC is considered a test article at this phase of its operational life, ISO 17566 is used as a normative reference in constructing the initialization plan. It provides SC manufacturers, operators and other stakeholders with a common language and form to verify and document spacecraft initialization prior to normal SC mission operations.

Space systems - Early operations - Part 2: Initialization plan

ISO 10784-1:2011 航天系统.早期运行.第1部分:宇宙飞船的初始化和调试

A general definition of initialization is that it begins at separation of the spacecraft (SC) from the launcher. In some cases, a more exact definition will be that initialization begins in flight, upon planned change in mode or state of the SC from the launch configuration. Commissioning is completed when the SC, including its payload, is certified for initial mission operations. Prior to certification for mission operations, the SC is described as a test article in the three parts of ISO 10784. ISO 10784 does not include a requirement for contingency plans, but does include a statement of the need for contingency planning. This part of ISO 10784 outlines general descriptive information for SC initialization and commissioning as might be appropriate for programme management, project engineering or programme test documentation. Since the SC is considered a test article at this phase of its operational life, ISO 17566 is used as a normative reference in constructing the initialization plan and the commissioning report. It provides SC manufacturers, SC operators and other stakeholders with a common language and form to verify and document spacecraft initialization and commissioning prior to normal SC mission operations.

Space systems - Early operations - Part 1: Spacecraft initialization and commissioning

ISO 10784-3:2011 航天系统.早期运行.第3部分:调试报告

A general definition of initialization is that it begins at separation of the spacecraft (SC) from the launcher. In some cases, a more exact definition will be that initialization begins in flight, upon planned change in mode or state of the SC from the launch configuration. Commissioning is completed when the SC, including its payload, is certified for initial mission operations. Prior to certification for mission operations, the SC is described as a test article in the three parts of ISO 10784. ISO 10784 does not include a requirement for contingency plans, but does include a statement of the need for contingency planning. This part of ISO 10784 outlines general descriptive information for SC initialization and commissioning as might be appropriate for programme management, project engineering or programme test documentation. Since the SC is considered a test article at this phase of its operational life, ISO 17566 is used as a normative reference in constructing the commissioning report. It provides SC manufacturers, SC operators and other stakeholders with a common language and form to verify and document spacecraft initialization and commissioning prior to normal SC mission operations.

Space systems - Early operations - Part 3: Commissioning report

BS ISO 24113:2011 航天系统.减轻太空垃圾的要求

Space systems. Space debris mitigation requirements

QJ 20062.1-2011 基于Patran/Nastran软件的航天产品结构有限元分析要求

Requirements for Finite Element Analysis of Aerospace Product Structure Based on Patran/Nastran Software

QJ 20062.5-2011 基于Patran/Nastran软件的航天产品结构有限元分析要求

本部分规定了使用 Patran/Nastran 软件对航天复合材料产品进行有限元分析时材料模型建立方法， 复合材料有限元分析的后处理等要求。 本部分适用于使用 Patran/Nastran 软件对航天复合材料产品结构进行有限元分析、数据及文档管理。

Requirements for Finite Element Analysis of Aerospace Product Structure Based on Patran/Nastran Software

QJ 20062.3-2011 基于Patran/Nastran软件的航天产品结构有限元分析要求

本部分规定了使用 Patran/Nastran 软件对发射车车架进行有限元分析的分析类型，建立车架有限元 模型的方法。 本部分适用于使用 Patran/Nastran 软件进行发射车车架结构有限元分析、数据及文档管理。使用其 他有限元软件进行其他功能车辆《(如装填车，转载车，运输车) 和车辆型式(半挂、全挂) 有限元分析 时可参照使用。

Requirements for Finite Element Analysis of Aerospace Product Structure Based on Patran/Nastran Software