V71 航天器总体 标准查询与下载

GB/T 29082-2012(英文版) 卫星存储要求

Storage requirements for satellite

GB/T 32307-2015(英文版) 航天器磁性能评估与控制方法

Assessment and control methods of spacecraft magnetic property

GB/T 29078-2012(英文版) 航天器发射窗设计导则

Design guidelines for spacecraft launch window

GB/T 29084-2012(英文版) 航天器的接地要求

Grounding requirements of spacecraft

BS ISO 17770:2017 空间系统 立方体卫星（立方体卫星）

Space systems. Cube satellites (CubeSats)

BS ISO 16699:2015 航天系统. 轨道发射阶段的处置工作

Space systems. Disposal of orbital launch stages

BS ISO 16164:2015 空间系统. 在或者跨越低地球轨道上运行的卫星处理

Space systems. Disposal of satellites operating in or crossing Low Earth Orbit

ISO 16164:2015 空间系统. 在或者跨越低地球轨道上运行的卫星处理

This International Standard focuses on the post-mission disposal of spacecraft operating in, or crossing, Low Earth Orbit (LEO). The disposal of orbital launch stages operating in, or crossing, LEO is not dealt with in this International Standard. Post-mission disposal of an Earth-orbiting spacecraft broadly means removing the spacecraft from its operational orbit after the end of mission, manoeuvring it to a region of space where it is less likely to interfere or collide with other operational spacecraft or with orbital debris and passivating. For a spacecraft operating in, or crossing LEO, there are six disposal options that might be used to ensure its compliance with orbital debris mitigation requirements (as stated in ISO 24113). In order of preference, these are the following: a) retrieving it and performing a controlled re-entry to recover it safely on the Earth; c) manoeuvring it in a controlled manner to an orbit that has a decay lifetime short enough to meet all orbital debris mitigation requirements; e) allowing its orbit to decay naturally, given that all orbital debris mitigation requirements will be met without the need for a disposal manoeuvre or other action; b) manoeuvring it in a controlled manner into a targeted re-entry with a well-defined impact footprint on the surface of the Earth to limit the possibility of human casualty; d) augmenting its orbital decay by deploying a device so that the remaining orbital lifetime is short enough to meet all orbital debris mitigation requirements; f) manoeuvring it in a controlled manner to an orbit with a perigee altitude sufficiently above the LEO protected region (i.e. a graveyard orbit) that long-term perturbation forces do not cause it to reenter the LEO protected region within 100 years. This International Standard specifies requirements for the following: a) planning for disposal and passivation of spacecraft operating in LEO to ensure that final disposal is sufficiently characterized and that adequate propellant will be reserved for any propulsive manoeuvre required, b) selecting a disposal orbit where the spacecraft will re-enter the Earth’s atmosphere within the next 25-years, or where the spacecraft will not re-enter the protected region within the next 100-years, and c) estimating, prior to launch, a 90 % or better probability of successfully executing the disposal manoeuvre. Techniques for planning and executing space hardware disposal are provided that reflect current internationally accepted guidelines and consider current operational procedures and best practices.

Space systems - Disposal of satellites operating in or crossing Low Earth Orbit

GOST R 56526-2015 具有活动操作长寿命的独特 (小系列) 生产的空间系统, 复合物以及无人航天器的可靠性和安全要求

Reliability and safety requirements for space systems, complexes and unmanned spacecraft of unique (small series) production with long life of active operation

GOST R 56516-2015 具有活动操作长寿命的独特 (小系列) 生产的空间系统, 复合物以及无人航天器可靠性和安全控制性的规则和程序

Regulations and procedures for reliability and safety control of space systems, complexes and unmanned spacecraft of unique (small series) production with long life of active operation

GOST R EN 13718-1-2015 医疗车辆及其设备. 救护飞机. 第1部分. 救护飞机中使用的医疗器械要求

Medical vehicles and their equipment. Air Ambulances. Part 1. Requirements for medical devices used in air ambulances

GOST R EN 13718-2-2015 医疗车辆及其设备. 救护飞机. 第2部分. 救护飞机的操作和技术要求

Medical vehicles and their equipment. Air ambulances. Part 2. Operational and technical requirements of air ambulances

GOST R 56525-2015 无人航天器. 运输的通用要求

Unmanned spacecrafts. General requirements for transportation

BS EN 16602-70-29:2014 航天产品保证. 载人航天器机组舱使用的材料和组装器件的脱气产品的测定

Space product assurance. Determination of offgassing products from materials and assembled articles to be used in a manned space vehicle crew compartment

BS EN 16603-50-14:2014 航天工程. 航天器离散接口

Space engineering. Spacecraft discrete interfaces

BS EN 16603-50-13:2014 航天工程. 机载航天器上MIL-STD-1553B数据总线的接口和通信协议

Space engineering. Interface and communication protocol for MIL-STD-1553B data bus onboard spacecraft

ANSI/NFPA 1122-2012 模拟火箭规程

1.1 Scope. 1.1.1 This code shall apply to the design, construction, limitation of rocket propellant mass and power, and reliability of model rocket motors and model rocket motor reloading kits and their components, produced commercially for sale to or for use by the public for purposes of education, recreation, and sporting competition. 1.1.2 This code also shall apply to the design and construction of model rockets propelled by model rocket motors specified in 1.1.1. 1.1.3 This code also shall apply to the conduct of launch operations of model rockets specified in 1.1.2. 1.1.4 This code shall not apply to the design, construction, production, manufacture, fabrication, maintenance, launch, flight, test, operation, use, or other activity that is connected with a rocket or rocket motor where carried out or engaged in by any of the following: (1) National, state, or local government (2) Individual, firm, partnership, joint venture, corporation, or other business entity engaged as a licensed business in the research, development, production, testing, maintenance, or supply of rockets, rocket motors, rocket propellant chemicals, or rocket components or parts (3) Colleges or universities 1.1.5 This code shall not apply to the design, construction, fabrication, maintenance, production, manufacture, launch, flight, test, operation, or use of rocket-propelled model aircraft that sustain their mass against the force of gravity by aerodynamic lifting surfaces that support the aircraft during the entire duration of its flight in the air, but shall apply to the model rocket motors and their components that provide the propulsion for such model aircraft. 1.1.6 This code shall not apply to model or toy rockets propelled by pressurized-liquid rocket motors containing less than 250 mL (8.45 fl oz) of water. 1.1.7 This code shall not apply to fireworks rockets or pyrotechnic rockets as defined in NFPA 1123, Code for Fireworks Display. 1.1.8 This code shall not apply to NFPA 1124, Code for the Manufacture, Transportation, Storage, and Retail Sales of Fireworks and Pyrotechnic Articles. 1.1.9 This code shall not apply to NFPA 1126, Standard for the Use of Pyrotechnics Before a Proximate Audience. 1.1.10 This code shall not apply to high power rocketry as defined in NFPA 1127, Code for High Power Rocketry.

Code for Model Rocketry

BS ISO 11221:2011 空间系统.空间太阳能板.宇宙飞船充电感应静电释放试验方法

Space systems. Space solar panels. Spacecraft charging induced electrostatic discharge test methods

QJ 20016-2011 液体火箭POGO振动分析与试验方法

本标准规定了液体运载火箭的POGO分析与试验的一般流程、POGO稳定性分析、动力系统相关参数获取、全箭振动特性参数获取和飞行试验验证。 本标准适用于液体运载火箭的POGO抑制设计和评估。

Pogo analysis and test method for liquid rocket

QJ 20051-2011 液体火箭发动机压力调节器通用规范

本规范规定了液体火箭发动机压力调节器的要求、质量保证规定和交货准备。 本规范适用于液体火箭发动机压力调节器（以下简称压调器）设计、生产、试验和验收。其它系统使用的压调器可参照使用。

General specification for pressure regulator of liquid rocket engine