BS ISO 24113-2011 Space systems Space debris mitigation requirements《航天系统 减轻太空垃圾的要求》.pdf

《BS ISO 24113-2011 Space systems Space debris mitigation requirements《航天系统 减轻太空垃圾的要求》.pdf》由会员分享，可在线阅读，更多相关《BS ISO 24113-2011 Space systems Space debris mitigation requirements《航天系统 减轻太空垃圾的要求》.pdf（26页珍藏版）》请在麦多课文档分享上搜索。

1、raising standards worldwideNO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBSI Standards PublicationBS ISO 24113:2011Space systems Space debrismitigation requirementsBS ISO 24113:2011 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of ISO 24113:2

2、011.Growth in the volume of space debris is of major international con-cern. The aim of ISO 24113 is to reduce this growth by setting out high level debris mitigation measures applicable to all elements of unmanned systems launched into, or passing through, near-Earth space, including launch vehicle

3、 orbital stages, operating spacecraft and any objects released as part of normal operations or disposal actions. These internationally agreed measures are derived from and are consistent with broader space debris mitigation guidelines published by organizations such as the Inter Agency Space Debris

4、Coordination Committee (IADC) and the United Nations Committee on the Peaceful Uses of Outer Space (UNCOPUOS).Global agreement that the growth in space debris needs to be reduced, and international consensus on the measures contained in ISO 24113 and associated lower level standards, offer a basis f

5、or a globally consistent approach to space debris mitigation. Measures for the mitigation of space debris can be adopted voluntarily, or be brought into effect through commercial contract, or incorporated as a condition in National regulation.UK nationals and entities incorporated in the UK which la

6、unch, pro-cure the launch or operate a space object or undertake any other activity in outer space must be licensed under the Outer Space Act 1986 (OSA). Before issuing a licence, the licensing authority currently the UK Space Agency assesses if the proposed space activity conforms to international

7、treaties (e.g. the requirements on liability and registration) and other applicable laws and regulations. A safety evaluation is required by the UK Space Agency before issuing a licence. The safety evaluation aims to determine whether a licence applicant can safely conduct the launch, operation and

8、disposal of a space system. In particular, the evaluation seeks to assess whether an applicant can demonstrate a clear understanding of the hazards involved, and that an appropriate risk management regime exists to limit those hazards. This is necessary to ensure that the activity will not jeopardiz

9、e public health or the safety of persons or property.The assessment carried out by the UK Space Agency also considers whether the proposed activity is compliant with international guidelines such as those relating to space debris mitigation. ISO 24113 and associated ISO debris mitigation standards p

10、rovide implementable and verifiable requirements that can be used by UK nationals or entities to demonstrate compliance with the broader debris mitigation guidelines mentioned above.As the implementation of debris mitigation measures can have a significant impact on the design and operation of space

11、 systems and consequently mission cost, it is clearly in the interest of those applying for a licence to confirm, at an early stage, which debris mitigation measures apply to their specific space system and with which the applicant must demonstrate compliance. ISO 24113 can be used as a basis for su

12、ch an assessment by the UK Space Agency prior to granting an applicant a licence pursuant to the OSA.BS ISO 24113:2011 BRITISH STANDARDThe UK participation in its preparation was entrusted to Technical Committee ACE/68/-/3, Space systems and operations - Operations and Ground Support.A list of organ

13、izations represented on this committee can be obtained on request to its secretary.This publication does not purport to include all the neces-sary provisions of a contract. Users are responsible for its correct application. BSI 2011ISBN 978 0 580 72707 8 ICS 49.140 Compliance with a British Standard

14、 cannot confer immunity from legal obligations.This British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 October 2011.Amendments issued since publicationDate T e x t a f f e c t e dBS ISO 24113:2011Reference numberISO 24113:2011(E)ISO 2011INTERNATIO

15、NAL STANDARD ISO24113Second edition2011-05-15Space systems Space debris mitigation requirements Systmes spatiaux Exigences de mitigation des dbris spatiaux BS ISO 24113:2011ISO 24113:2011(E) COPYRIGHT PROTECTED DOCUMENT ISO 2011 All rights reserved. Unless otherwise specified, no part of this public

16、ation may be reproduced or utilized in any form or by any means, electronic or mechanical, including photocopying and microfilm, without permission in writing from either ISO at the address below or ISOs member body in the country of the requester. ISO copyright office Case postale 56 CH-1211 Geneva

17、 20 Tel. + 41 22 749 01 11 Fax + 41 22 749 09 47 E-mail copyrightiso.org Web www.iso.org Published in Switzerland ii ISO 2011 All rights reservedBS ISO 24113:2011ISO 24113:2011(E) ISO 2011 All rights reserved iiiContents Page Foreword iv Introduction.v 1 Scope1 2 Normative references1 3 Terms and de

18、finitions .1 4 Symbols and abbreviated terms 3 4.1 Symbols3 4.2 Abbreviated terms .3 5 Protected regions 4 5.1 General .4 5.2 LEO protected region4 5.3 GEO protected region .4 6 Technical requirements 5 6.1 Avoiding the intentional release of space debris into Earth orbit during normal operations.5

19、6.2 Avoiding break-ups in Earth orbit .5 6.3 Removing a spacecraft or launch vehicle orbital stage from the protected regions after end of mission .5 7 Space debris mitigation plan7 Annex A (informative) Probability of successful disposal .8 Annex B (informative) Post-launch life cycle phases of a l

20、aunch vehicle or spacecraft 11 Bibliography13 BS ISO 24113:2011ISO 24113:2011(E) iv ISO 2011 All rights reservedForeword ISO (the International Organization for Standardization) is a worldwide federation of national standards bodies (ISO member bodies). The work of preparing International Standards

21、is normally carried out through ISO technical committees. Each member body interested in a subject for which a technical committee has been established has the right to be represented on that committee. International organizations, governmental and non-governmental, in liaison with ISO, also take pa

22、rt in the work. ISO collaborates closely with the International Electrotechnical Commission (IEC) on all matters of electrotechnical standardization. International Standards are drafted in accordance with the rules given in the ISO/IEC Directives, Part 2. The main task of technical committees is to

23、prepare International Standards. Draft International Standards adopted by the technical committees are circulated to the member bodies for voting. Publication as an International Standard requires approval by at least 75 % of the member bodies casting a vote. Attention is drawn to the possibility th

24、at some of the elements of this document may be the subject of patent rights. ISO shall not be held responsible for identifying any or all such patent rights. ISO 24113 was prepared by Technical Committee ISO/TC 20, Aircraft and space vehicles, Subcommittee SC 14, Space systems and operations. This

25、second edition cancels and replaces the first edition (ISO 24113:2010), of which it constitutes a minor revision. BS ISO 24113:2011ISO 24113:2011(E) ISO 2011 All rights reserved vIntroduction Space debris comprises all non-functional, man-made objects, including fragments and elements thereof, in Ea

26、rth orbit or re-entering the Earths atmosphere. The growing population of these objects poses an increasing hazard to missions. In response to this problem, there is international consensus that space activities need to be managed to minimize debris generation and risk. This consensus is embodied in

27、 space debris mitigation guidelines published by organizations such as the International Telecommunication Union (ITU)1, the Inter-Agency Space Debris Coordination Committee (IADC)23and the United Nations (UN)4. The transformation of debris mitigation guidelines into engineering practice is a key pu

28、rpose of this International Standard. The importance of this International Standard can be seen within the context of four UN treaties5that were established under the United Nations Committee on the Peaceful Uses of Outer Space (UNCOPUOS) to govern the involvement of nations in space activities. The

29、se are the Outer Space Treaty, the Liability Convention, the Registration Convention and the Rescue Agreement. Through some of these treaties, a Launching State has total liability for damage caused by its spacecraft or launch vehicle orbital stages (or any parts thereof) on the surface of the Earth

30、 or to aircraft in flight, as well as in outer space where fault can be proven. All countries are encouraged to abide by these international agreements in order not to endanger or constrain existing and future space missions. A Launching State can choose to appoint licensing or regulatory authoritie

31、s to administer its approach for complying with the above-mentioned UN treaties. In several Launching States, these authorities have implemented national legislation to enforce the UN treaties. Such legislation can include the mitigation of space debris. Some Launching States meet their obligations

32、by appointing non-regulatory government bodies, such as national space agencies, to provide the necessary guidelines or requirements, including those for space debris mitigation. The general aim of space debris mitigation is to reduce the growth of space debris by ensuring that spacecraft and launch

33、 vehicle orbital stages are designed, operated and disposed of in a manner that prevents them from generating debris throughout their orbital lifetime. This is achieved by the following actions: a) avoiding the intentional release of space debris into Earth orbit during normal operations; b) avoidin

34、g break-ups in Earth orbit; c) removing spacecraft and launch vehicle orbital stages from protected orbital regions after end of mission; d) performing the necessary actions to minimize the risk of collision with other space objects. Such actions are especially important for a spacecraft or launch v

35、ehicle orbital stage that has one or more of the following characteristics: a large collision cross-section; remains in orbit for many years; operates near manned mission orbital regions; operates in highly utilized regions, such as protected regions; operates in regions of high debris population. T

36、his International Standard transforms these objectives into a set of high-level debris mitigation requirements. Methods and processes to enable compliance with these requirements are provided in a series of lower-level implementation standards. BS ISO 24113:2011BS ISO 24113:2011INTERNATIONAL STANDAR

37、D ISO 24113:2011(E) ISO 2011 All rights reserved 1Space systems Space debris mitigation requirements 1 Scope This International Standard defines the primary space debris mitigation requirements applicable to all elements of unmanned systems launched into, or passing through, near-Earth space, includ

38、ing launch vehicle orbital stages, operating spacecraft and any objects released as part of normal operations or disposal actions. The requirements contained in this International Standard are intended to reduce the growth of space debris by ensuring that spacecraft and launch vehicle orbital stages

39、 are designed, operated and disposed of in a manner that prevents them from generating debris throughout their orbital lifetime. This International Standard is the top-level standard in a family of standards addressing debris mitigation. It will be the main interface for the user, bridging between t

40、he primary debris mitigation requirements and the lower-level implementation standards that will ensure compliance. This International Standard does not cover launch phase safety for which specific rules are defined elsewhere. 2 Normative references The following referenced documents are indispensab

41、le for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. ISO 9000:2005, Quality management systems Fundamentals and vocabulary 3 Terms and definitions For t

42、he purposes of this document, the terms and definitions given in ISO 9000:2005 and the following apply. 3.1 approving agent entity from whom approval is sought for the implementation of space debris mitigation requirements with respect to the procurement of a spacecraft, or its launch, or its operat

43、ions in space, or a combination of those activities EXAMPLE Regulatory or licensing authorities; national or international space agencies. 3.2 break-up event that destroys an object and generates fragments that are released into space 3.3 casualty risk probability that a person is killed or seriousl

44、y injured BS ISO 24113:2011ISO 24113:2011(E) 2 ISO 2011 All rights reserved3.4 disposal actions performed by a spacecraft or launch vehicle orbital stage to permanently reduce its chance of accidental break-up and to achieve its required long-term clearance of the protected regions 3.5 disposal phas

45、e interval during which a spacecraft or launch vehicle orbital stage completes its disposal actions 3.6 end of life instant when a spacecraft or launch vehicle orbital stage is permanently turned off, nominally as it completes its disposal phase, or when it re-enters, or when the operator can no lon

46、ger control it 3.7 end of mission instant when a spacecraft or launch vehicle orbital stage completes the tasks or functions for which it has been designed, or when it becomes non-functional or permanently halted because of a failure or because of a voluntary decision 3.8 geostationary Earth orbit G

47、EO Earth orbit having zero inclination and zero eccentricity, whose orbital period is equal to the Earths sidereal rotation period 3.9 launch vehicle orbital stage stage of a launch vehicle that is designed to achieve orbit 3.10 Launching State State that launches or procures the launching of a spac

48、ecraft, or a State from whose territory or facility a spacecraft is launched NOTE This definition is consistent with the definition in the UN Liability Convention5and Resolution 59/1156of 10 December 2004 on the notion of the Launching State. 3.11 normal operations planned tasks or functions perform

49、ed by a spacecraft or launch vehicle orbital stage prior to its disposal 3.12 orbital lifetime period of time from when a spacecraft or launch vehicle orbital stage achieves Earth orbit to when it commences re-entry 3.13 probability of successful disposal probability of successfully disposing of a spacecraft or launch vehicle orbital stage, evaluated as a conditional probability weighted on the mission success at the time disposal is executed NOTE See Annex A. 3.14 protected region region in space that is protected w