V71 航天器总体 标准查询与下载
共找到 368 条与 航天器总体 相关的标准，共 25 页
本标准规定了飞行中运载火箭末级剩余推进剂排放的设计准则、排放方式选择等一般设计要求、详细设计要求和效果评估等内容。 本标准适用于采用常温液体推进剂和低温液体推进剂的运载火箭末级剩余推进剂排放设计，运载火箭上面级等的剩余推进剂处理相关设计可参照执行。
Design requirements for residual propellant venting of launch vehicle
- ICS
- 49.020
- CCS
- V71
- 发布
- 2015-12-31
- 实施
- 2016-07-01
Requirements for postmission disposal of GEO satellites
- ICS
- CCS
- V71
- 发布
- 2015-12-31
- 实施
- 2016-07-01
Design requirements for residual propellant venting of launch vehicle
- ICS
- CCS
- V71
- 发布
- 2015-12-31
- 实施
- 2016-07-01
本标准规定了航天器磁性评估和磁性控制的目的、程序和方法。 本标准适用于航天器及其部、组件的磁性评估和磁性控制。
Assessment and control methods of spacecraft magnetic property
- ICS
- 49.060
- CCS
- V71
- 发布
- 2015-12-31
- 实施
- 2016-07-01
Assessment and control methods of spacecraft magnetic property
- ICS
- CCS
- V71
- 发布
- 实施
Space systems. Cube satellites (CubeSats)
- ICS
- 49.140
- CCS
- V71
- 发布
- 2017-07-10
- 实施
- 2017-07-10
Space systems. Disposal of orbital launch stages
- ICS
- 49.140
- CCS
- V71
- 发布
- 2015-12-31
- 实施
- 2015-12-31
Space systems. Disposal of satellites operating in or crossing Low Earth Orbit
- ICS
- 49.140
- CCS
- V71
- 发布
- 2015-07-31
- 实施
- 2015-07-31
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
- ICS
- 49.140
- CCS
- V71
- 发布
- 2015-07
- 实施
Medical vehicles and their equipment. Air ambulances. Part 2. Operational and technical requirements of air ambulances
- ICS
- 11.040.01;11.160
- CCS
- V71
- 发布
- 2015
- 实施
- 2016-09-01
Reliability and safety requirements for space systems, complexes and unmanned spacecraft of unique (small series) production with long life of active operation
- ICS
- 49.140
- CCS
- V71
- 发布
- 2015
- 实施
- 2016-04-01
Medical vehicles and their equipment. Air Ambulances. Part 1. Requirements for medical devices used in air ambulances
- ICS
- 11.040.01;11.160
- CCS
- V71
- 发布
- 2015
- 实施
- 2016-09-01
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
- ICS
- 49.140
- CCS
- V71
- 发布
- 2015
- 实施
- 2016-01-01
Unmanned spacecrafts. General requirements for transportation
- ICS
- 49.140
- CCS
- V71
- 发布
- 2015
- 实施
- 2016-01-01
Space product assurance. Determination of offgassing products from materials and assembled articles to be used in a manned space vehicle crew compartment
- ICS
- 49.140
- CCS
- V71
- 发布
- 2014-11-30
- 实施
- 2014-11-30
Space engineering. Spacecraft discrete interfaces
- ICS
- 49.140
- CCS
- V71
- 发布
- 2014-09-30
- 实施
- 2014-09-30
Space engineering. Interface and communication protocol for MIL-STD-1553B data bus onboard spacecraft
- ICS
- 49.140
- CCS
- V71
- 发布
- 2014-09-30
- 实施
- 2014-09-30
