SIST EN 302 186 V2.1.1:2016
(Main)Satellite Earth Stations and Systems (SES) - Harmonised Standard for satellite mobile Aircraft Earth Stations (AESs) operating in the 11/12/14 GHz frequency bands covering the essential requirements of article 3.2 of the Directive 2014/53/EU
Satellite Earth Stations and Systems (SES) - Harmonised Standard for satellite mobile Aircraft Earth Stations (AESs) operating in the 11/12/14 GHz frequency bands covering the essential requirements of article 3.2 of the Directive 2014/53/EU
The present document specifies certain minimum technical performance requirements of Aircraft Earth Station (AES) equipment with both transmit and receive capabilities for provision of aeronautical mobile satellite service, in the frequency bands given in table 1.
The AES has the following characteristics:
• These AESs are equipment for installation on aircraft.
• The AES could consist of a number of modules from the antenna subsystem to the user interfaces.
• The AES uses linear polarization.
• The AES system uses digital modulation.
• The AES operates through a GSO satellite at least 3° away from any other geostationary satellite operating in the same frequency band and covering the same area.
• The antenna of the AES is directional, with means of tracking the satellites, which can be achieved by using either an active phase array or reflective type configuration.
• These AESs are operating as part of a satellite network used for the distribution and/or exchange of
information between users.
• These AESs are controlled and monitored by a Network Control Facility (NCF). The NCF is outside the scope of the present document.
• When on the ground, the AES does not transmit at elevation angles below 7o with respect to the local horizontal plane, except at locations where transmissions below 7o are permitted by the local Administration; (the minimum elevation angle is also limited as per clause 4.2).
The technical requirements in the present document are in two major categories:
• emission limits: to protect other radio services and systems from harmful interference generated by the AES in normal use;
• AES Control and Monitoring Functions (CMF): to protect other radio services and systems from unwanted transmissions from the AES. The CMF in each AES is capable of answering to commands from the Network Control Facility (NCF) for its supporting satellite network.
The present document applies to the AESs with their ancillary equipment and its various ports, and when operated within the boundary limits of the operational environmental profile declared by the manufacturer.
The technical requirements for the AES in regard to the Power Flux Density (PFD) limits to protect Fixed Service (FS) and Radio Astronomy Service (RAS) are based on annexes B and C of Recommendation ITU-R M.1643 [5] and ECC Report 26 [i.4]. Furthermore, in relation to the protection of the Fixed Satellite Service (FSS) the technical requirements of the AES take into account annex A of Recommendation ITU-R M.1643 [5].
The present document is intended to cover the provisions of Directive 2014/53/EU [6] (RE Directive) article 3.2, which states that "… radio equipment shall be so constructed that it both effectively and supports the use of radio spectrum allocated in order to avoid harmful interference".
In addition to the present document, other ENs that specify technical requirements in respect of essential requirements of other parts of article 3 of the RE Directive [6] may apply to equipment within the scope of the present document.
NOTE: A list of such ENs is included on the web site at: http:\\www.newapproach.org.
The present document does not cover equipment compliance with relevant civil aviation regulations. In this respect, an AES, for its installation and operation on board an aircraft is subject to additional national or international civil aviation airworthiness certification requirements, for example to EUROCAE ED-14D [4].
Satelitske zemeljske postaje in sistemi (SES) - Harmonizirani standard, ki zajema bistvene zahteve člena 3.2 direktive 2014/53/EU, za satelitske mobilne letalske zemeljske postaje (AES), delujoče v frekvenčnih pasovih 11/12/14 GHz
Ta dokument določa minimalne zahteve v zvezi s tehnično zmogljivostjo opreme letalske zemeljske postaje (AES) s sposobnostjo oddajanja in sprejemanja za zagotavljanje letalske mobilne satelitske storitve v frekvenčnih pasovih, navedenih v preglednici 1.
Letalske zemeljske postaje morajo imeti naslednje lastnosti:
• Letalske zemeljske postaje so oprema, namenjena montaži na letalo.
• Letalske zemeljske postaje so lahko sestavljene iz več modulov, od antenskega podsistema do uporabniških vmesnikov.
• Letalska zemeljska postaja uporablja linearno polarizacijo.
• Sistem letalske zemeljske postaje uporablja digitalno modulacijo.
• Letalska zemeljska postaja deluje prek geostacionarnega satelita, ki je odmaknjen za vsaj 3° od kateregakoli drugega geostacionarnega satelita, ki deluje v istem frekvenčnem pasu in na istem območju.
• Antena letalske zemeljske postaje je usmerjena z možnostjo sledenja satelitu, kar je mogoče doseči z uporabo aktivnega faznega polja ali odbojne konfiguracije.
• Letalske zemeljske postaje delujejo kot del satelitskega omrežja, ki se uporablja za distribucijo in/ali izmenjavo
informacij med uporabniki;
• Letalske zemeljske postaje se krmilijo in spremljajo z napravo za krmiljenje omrežja (NCF). Naprava za krmiljenje omrežja ne spada v področje uporabe tega dokumenta.
• Letalska zemeljska postaja na tleh ne oddaja pod višinskim kotom, manjšim od 7°, glede na lokalno vodoravno površino, razen na območjih, kjer lokalna uprava dovoljuje oddajanje pod kotom, manjšim od 7° (najmanjši višinski kot je tudi omejen v točki 4.2).
Tehnične zahteve v tem dokumentu so razvrščene v dve večji kategoriji:
• Omejitve emisij: za zaščito drugih radijskih storitev in sistemov pred škodljivimi motnjami, ki jih povzroča letalska zemeljska postaja pri običajni uporabi.
• Funkcije letalske zemeljske postaje za krmiljenje in spremljanje (CMF): za zaščito drugih radijskih storitev in sistemov pred neželenim oddajanjem letalske zemeljske postaje. Funkcije za krmiljenje in spremljanje v vsaki letalski zemeljski postaji se lahko odzivajo na ukaze naprave za krmiljenje omrežja (NCF) podpornega satelitskega omrežja.
Ta dokument se uporablja za letalske zemeljske postaje s pomožno opremo in različnimi zemeljskimi vrati, ko ta deluje znotraj mejnih vrednosti obratovalnega okoljskega profila, kot ga določi proizvajalec.
Tehnične zahteve za letalsko zemeljsko postajo glede omejitve gostote pretoka moči (PFD) za zaščito fiksnih storitev (FS) in storitve radijske astronomije (RAS) temeljijo na dodatkih B in C priporočila ITU-R M.1643 [5] in poročila ECC 26 [i.4]. Poleg tega tehnične zahteve za letalske zemeljske postaje v zvezi z zaščito fiksnih satelitskih storitev (FSS) upoštevajo dodatek A priporočila ITU-R M.1643 [5].
Ta dokument zajema določbe člena 3.2 Direktive 2014/53/EU [6] (direktive RE), ki navaja: »/.../ Radijska oprema je izdelana tako, da optimalno uporablja in podpira učinkovito izrabo radijskega spektra, z namenom preprečevanja škodljivega motenja.«
Poleg tega dokumenta se za opremo v področju uporabe tega dokumenta uporabljajo tudi drugi standardi EN, ki določajo tehnične zahteve v zvezi z bistvenimi zahtevami iz drugih delov člena 3 direktive RE [6].
OPOMBA: seznam tovrstnih standardov EN je na voljo na spletnem mestu http:\\www.newapproach.org.
Ta dokument ne zajema skladnosti opreme z ustreznimi predpisi civilnega letalstva. Tako sta montaža in delovanje letalske zemeljske postaje na krovu letala predmet dodatnih zahtev nacionalnega ali mednarodnega civilnega letalstva za potrjevanje plovnosti, na primer EUROCAE ED-14D [4].
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2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.*+]Satellite Earth Stations and Systems (SES) - Harmonised Standard for satellite mobile Aircraft Earth Stations (AESs) operating in the 11/12/14 GHz frequency bands covering the essential requirements of article 3.2 of the Directive 2014/53/EU33.060.30Radiorelejni in fiksni satelitski komunikacijski sistemiRadio relay and fixed satellite communications systemsICS:Ta slovenski standard je istoveten z:ETSI EN 302 186 V2.1.1 (2016-05)SIST EN 302 186 V2.1.1:2016en01-september-2016SIST EN 302 186 V2.1.1:2016SLOVENSKI
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SIST EN 302 186 V2.1.1:2016
ETSI EN 302 186 V2.1.1 (2016-05) Satellite Earth Stations and Systems (SES); Harmonised Standard for satellite mobile Aircraft Earth Stations (AESs) operating in the 11/12/14 GHz frequency bands covering the essential requirements of article 3.2 of the Directive 2014/53/EU
HARMONISED EUROPEAN STANDARD SIST EN 302 186 V2.1.1:2016
ETSI ETSI EN 302 186 V2.1.1 (2016-05) 2
Reference REN/SES-00392 Keywords aeronautical, air interface, AMSS, earth station, FSS, GSO, mobile, MSS, regulation, satellite ETSI 650 Route des Lucioles F-06921 Sophia Antipolis Cedex - FRANCE
Tel.: +33 4 92 94 42 00
Fax: +33 4 93 65 47 16
Siret N° 348 623 562 00017 - NAF 742 C Association à but non lucratif enregistrée à la Sous-Préfecture de Grasse (06) N° 7803/88
Important notice The present document can be downloaded from: http://www.etsi.org/standards-search The present document may be made available in electronic versions and/or in print. The content of any electronic and/or print versions of the present document shall not be modified without the prior written authorization of ETSI. In case of any existing or perceived difference in contents between such versions and/or in print, the only prevailing document is the print of the Portable Document Format (PDF) version kept on a specific network drive within ETSI Secretariat. Users of the present document should be aware that the document may be subject to revision or change of status. Information on the current status of this and other ETSI documents is available at https://portal.etsi.org/TB/ETSIDeliverableStatus.aspx If you find errors in the present document, please send your comment to one of the following services: https://portal.etsi.org/People/CommiteeSupportStaff.aspx Copyright Notification No part may be reproduced or utilized in any form or by any means, electronic or mechanical, including photocopying and microfilm except as authorized by written permission of ETSI. The content of the PDF version shall not be modified without the written authorization of ETSI. The copyright and the foregoing restriction extend to reproduction in all media.
© European Telecommunications Standards Institute 2016. All rights reserved.
DECTTM, PLUGTESTSTM, UMTSTM and the ETSI logo are Trade Marks of ETSI registered for the benefit of its Members. 3GPPTM and LTE™ are Trade Marks of ETSI registered for the benefit of its Members and of the 3GPP Organizational Partners. GSM® and the GSM logo are Trade Marks registered and owned by the GSM Association. SIST EN 302 186 V2.1.1:2016
ETSI ETSI EN 302 186 V2.1.1 (2016-05) 3 Contents Intellectual Property Rights . 7 Foreword . 7 Modal verbs terminology . 7 Introduction . 7 1 Scope . 9 2 References . 10 2.1 Normative references . 10 2.2 Informative references . 10 3 Definitions, symbols and abbreviations . 11 3.1 Definitions . 11 3.2 Symbols . 14 3.3 Abbreviations . 14 4 Technical requirement specifications . 15 4.1 General . 15 4.1.0 Introduction. 15 4.1.1 Environmental profile . 16 4.2 Conformance requirements . 16 4.2.1 General . 16 4.2.2 Spurious radiation . 16 4.2.2.1 Justification . 16 4.2.2.2 Specification. 16 4.2.2.3 Conformance tests . 17 4.2.3 On-axis spurious radiation . 17 4.2.3.1 Justification . 17 4.2.3.2 Specification. 17 4.2.3.2.1 "Carrier-on" state . 17 4.2.3.2.2 "Carrier-off" state and "transmission disabled" state . 18 4.2.3.3 Conformance tests . 18 4.2.4 Off-axis EIRP emissions density in the nominated bandwidth . 18 4.2.4.1 Justification . 18 4.2.4.2 Specification. 18 4.2.4.3 Conformance tests . 19 4.2.5 Control and Monitoring Functions (CMF) . 19 4.2.5.0 General . 19 4.2.5.1 Processor monitoring . 20 4.2.5.1.1 Justification . 20 4.2.5.1.2 Specification . 20 4.2.5.1.3 Conformance tests . 21 4.2.5.2 Transmit subsystem monitoring . 21 4.2.5.2.1 Justification . 21 4.2.5.2.2 Specification . 21 4.2.5.2.3 Conformance tests . 21 4.2.5.3 Power-on/Reset . 21 4.2.5.3.1 Justification . 21 4.2.5.3.2 Specification . 21 4.2.5.3.3 Conformance tests . 21 4.2.5.4 Control Channel (CC) reception . 21 4.2.5.4.1 Justification . 21 4.2.5.4.2 Specification . 21 4.2.5.4.3 Conformance tests . 21 4.2.5.5 Network control commands . 22 4.2.5.5.1 Justification . 22 4.2.5.5.2 Specification . 22 4.2.5.5.3 Conformance tests . 22 SIST EN 302 186 V2.1.1:2016
ETSI ETSI EN 302 186 V2.1.1 (2016-05) 4 4.2.5.6 Initial burst transmission . 22 4.2.5.6.1 General . 22 4.2.5.6.2 Specification . 22 4.2.5.6.3 Conformance tests . 23 4.2.6 Power Flux Density at the surface of the earth . 23 4.2.6.1 General . 23 4.2.6.2 Power flux density limits in the 14,00 GHz to 14,50 GHz frequency band . 23 4.2.6.2.1 Justification . 23 4.2.6.2.2 Specification 1: Mode of PFD limitation . 23 4.2.6.2.3 Specification 2: Location where to limit the PFD . 24 4.2.6.2.4 Specification 3: PFD limitation . 24 4.2.6.2.5 Specification 4: Fault conditions . 25 4.2.6.2.6 Conformance tests . 25 4.2.7 Receive antenna off-axis gain pattern . 25 4.2.7.1 Justification . 25 4.2.7.2 Specification. 25 4.2.7.3 Conformance tests . 26 4.2.8 Blocking performance . 26 4.2.8.1 Justification . 26 4.2.8.2 Specification. 26 4.2.8.3 Conformance tests . 26 4.2.9 Adjacent Signal Selectivity . 26 4.2.9.1 Justification . 26 4.2.9.2 Specification. 26 4.2.9.3 Conformance tests . 27 5 Testing for compliance with technical requirements . 27 5.1 Environmental conditions for testing . 27 5.2 Essential radio test suites . 27 6 Test methods . 27 6.0 General . 27 6.1 Spurious radiation. 28 6.1.1 Test method . 28 6.1.1.0 Introduction . 28 6.1.1.1 Up to 1 000 MHz (see clause 4.2.2.2, table 2) . 29 6.1.1.1.1 Test site. 29 6.1.1.1.2 Measuring receivers . 29 6.1.1.1.3 Procedure . 29 6.1.1.2 Above 1 000 MHz (see clause 4.2.2.2, tables 3 and 4) . 29 6.1.1.2.0 General . 29 6.1.1.2.1 Identification of the significant frequencies of spurious radiation . 30 6.1.1.2.2 Measurement of radiated power levels of identified spurious radiation . 30 6.2 On-axis spurious radiation . 31 6.2.1 Test method . 31 6.2.1.1 Test site . 31 6.2.1.2 Method of measurement . 31 6.2.1.2.1 General . 31 6.2.1.2.2 Method of measurement at the antenna flange . 32 6.2.1.2.3 Method of measurement with a test antenna . 32 6.3 Off-axis EIRP emissions density in the nominated bandwidth . 33 6.3.1 General . 33 6.3.2 rms antenna pointing accuracy. 34 6.3.2.1 Method of measurement . 34 6.3.3 Measurement of the off-axis EIRP without the antenna . 35 6.3.3.1 Transmitter output power density . 35 6.3.3.1.0 General . 35 6.3.3.1.1 Method of measurement . 35 6.3.3.2 Antenna transmit gain . 35 6.3.3.2.1 General . 35 6.3.3.2.2 Test site. 35 6.3.3.2.3 Method of measurement . 36 SIST EN 302 186 V2.1.1:2016
ETSI ETSI EN 302 186 V2.1.1 (2016-05) 5 6.3.3.3 Antenna transmit radiation patterns . 37 6.3.3.3.1 General . 37 6.3.3.3.2 Test site. 37 6.3.3.3.3 Method of measurement . 37 6.3.3.4 Computation of results . 38 6.3.4 Measurement of the off-axis EIRP with the antenna . 38 6.3.4.1 General . 38 6.3.4.2 Maximum EIRP density per 40 kHz ratio relative to the EIRP . 38 6.3.4.2.0 General . 38 6.3.4.2.1 Method of measurement . 38 6.3.4.3 Maximum on-axis EIRP . 39 6.3.4.3.1 General . 39 6.3.4.3.2 Test site. 39 6.3.4.3.3 Method of measurement . 39 6.3.4.4 Antenna transmit radiation patterns . 41 6.3.4.4.1 General . 41 6.3.4.4.2 Test site. 41 6.3.4.4.3 Method of measurement . 41 6.3.4.5 Computation of results . 42 6.4 Power Flux Density Test . 42 6.4.1 General . 42 6.4.2 Verification of specification 1: Mode of PFD limitation . 43 6.4.3 Verification of specification 2: Location where to limit the PFD . 43 6.4.4 Verification of specification 3: PFD limitation . 43 6.4.4.1 Measurement of the antenna radiation pattern below the aircraft fuselage . 43 6.4.4.1.1 General . 43 6.4.4.1.2 Test site. 43 6.4.4.1.3 Test method procedure . 43 6.4.4.2 Measurement of on-axis EIRP as a function of altitude . 44 6.4.4.2.1 General . 44 6.4.4.2.2 Test site. 45 6.4.4.2.3 Method of measurement with a test antenna . 45 6.4.4.3 Computation of the power flux density at the surface of the Earth . 46 6.4.5 Verification of specification 4: Fault conditions . 46 6.4.5.1 Test Arrangement . 46 6.4.5.2 Test method . 46 6.5 Control and monitoring . 47 6.5.0 General . 47 6.5.1 Test arrangement . 47 6.5.2 Processor monitoring . 48 6.5.2.1 Test method . 48 6.5.3 Transmit subsystem monitoring . 48 6.5.3.1 Test method . 48 6.5.4 Power-on/Reset . 49 6.5.4.1 Test method . 49 6.5.5 Control Channel (CC) reception . 49 6.5.5.1 Test method . 49 6.5.6 Network control commands . 50 6.5.6.1 Test method . 50 6.5.7 Initial burst transmission . 51 6.5.7.1 Test method . 51 6.6 Receive antenna off-axis gain pattern . 51 6.6.1 Test method . 51 6.6.1.1 Test site . 51 6.6.1.2 Method of measurement . 52 6.6.1.3 Computation .
...
ETSI EN 302 186 V2.1.1 (2016-05)
HARMONISED EUROPEAN STANDARD
Satellite Earth Stations and Systems (SES);
Harmonised Standard for satellite mobile
Aircraft Earth Stations (AESs)
operating in the 11/12/14 GHz frequency bands
covering the essential requirements
of article 3.2 of the Directive 2014/53/EU
---------------------- Page: 1 ----------------------
2 ETSI EN 302 186 V2.1.1 (2016-05)
Reference
REN/SES-00392
Keywords
aeronautical, air interface, AMSS, earth station,
FSS, GSO, mobile, MSS, regulation, satellite
ETSI
650 Route des Lucioles
F-06921 Sophia Antipolis Cedex - FRANCE
Tel.: +33 4 92 94 42 00 Fax: +33 4 93 65 47 16
Siret N° 348 623 562 00017 - NAF 742 C
Association à but non lucratif enregistrée à la
Sous-Préfecture de Grasse (06) N° 7803/88
Important notice
The present document can be downloaded from:
http://www.etsi.org/standards-search
The present document may be made available in electronic versions and/or in print. The content of any electronic and/or
print versions of the present document shall not be modified without the prior written authorization of ETSI. In case of any
existing or perceived difference in contents between such versions and/or in print, the only prevailing document is the
print of the Portable Document Format (PDF) version kept on a specific network drive within ETSI Secretariat.
Users of the present document should be aware that the document may be subject to revision or change of status.
Information on the current status of this and other ETSI documents is available at
https://portal.etsi.org/TB/ETSIDeliverableStatus.aspx
If you find errors in the present document, please send your comment to one of the following services:
https://portal.etsi.org/People/CommiteeSupportStaff.aspx
Copyright Notification
No part may be reproduced or utilized in any form or by any means, electronic or mechanical, including photocopying
and microfilm except as authorized by written permission of ETSI.
The content of the PDF version shall not be modified without the written authorization of ETSI.
The copyright and the foregoing restriction extend to reproduction in all media.
© European Telecommunications Standards Institute 2016.
All rights reserved.
TM TM TM
DECT , PLUGTESTS , UMTS and the ETSI logo are Trade Marks of ETSI registered for the benefit of its Members.
TM
3GPP and LTE™ are Trade Marks of ETSI registered for the benefit of its Members and
of the 3GPP Organizational Partners.
GSM® and the GSM logo are Trade Marks registered and owned by the GSM Association.
ETSI
---------------------- Page: 2 ----------------------
3 ETSI EN 302 186 V2.1.1 (2016-05)
Contents
Intellectual Property Rights . 7
Foreword . 7
Modal verbs terminology . 7
Introduction . 7
1 Scope . 9
2 References . 10
2.1 Normative references . 10
2.2 Informative references . 10
3 Definitions, symbols and abbreviations . 11
3.1 Definitions . 11
3.2 Symbols . 14
3.3 Abbreviations . 14
4 Technical requirement specifications . 15
4.1 General . 15
4.1.0 Introduction. 15
4.1.1 Environmental profile . 16
4.2 Conformance requirements . 16
4.2.1 General . 16
4.2.2 Spurious radiation . 16
4.2.2.1 Justification . 16
4.2.2.2 Specification. 16
4.2.2.3 Conformance tests . 17
4.2.3 On-axis spurious radiation . 17
4.2.3.1 Justification . 17
4.2.3.2 Specification. 17
4.2.3.2.1 "Carrier-on" state . 17
4.2.3.2.2 "Carrier-off" state and "transmission disabled" state . 18
4.2.3.3 Conformance tests . 18
4.2.4 Off-axis EIRP emissions density in the nominated bandwidth . 18
4.2.4.1 Justification . 18
4.2.4.2 Specification. 18
4.2.4.3 Conformance tests . 19
4.2.5 Control and Monitoring Functions (CMF) . 19
4.2.5.0 General . 19
4.2.5.1 Processor monitoring . 20
4.2.5.1.1 Justification . 20
4.2.5.1.2 Specification . 20
4.2.5.1.3 Conformance tests . 21
4.2.5.2 Transmit subsystem monitoring . 21
4.2.5.2.1 Justification . 21
4.2.5.2.2 Specification . 21
4.2.5.2.3 Conformance tests . 21
4.2.5.3 Power-on/Reset . 21
4.2.5.3.1 Justification . 21
4.2.5.3.2 Specification . 21
4.2.5.3.3 Conformance tests . 21
4.2.5.4 Control Channel (CC) reception . 21
4.2.5.4.1 Justification . 21
4.2.5.4.2 Specification . 21
4.2.5.4.3 Conformance tests . 21
4.2.5.5 Network control commands . 22
4.2.5.5.1 Justification . 22
4.2.5.5.2 Specification . 22
4.2.5.5.3 Conformance tests . 22
ETSI
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4 ETSI EN 302 186 V2.1.1 (2016-05)
4.2.5.6 Initial burst transmission . 22
4.2.5.6.1 General . 22
4.2.5.6.2 Specification . 22
4.2.5.6.3 Conformance tests . 23
4.2.6 Power Flux Density at the surface of the earth . 23
4.2.6.1 General . 23
4.2.6.2 Power flux density limits in the 14,00 GHz to 14,50 GHz frequency band . 23
4.2.6.2.1 Justification . 23
4.2.6.2.2 Specification 1: Mode of PFD limitation . 23
4.2.6.2.3 Specification 2: Location where to limit the PFD . 24
4.2.6.2.4 Specification 3: PFD limitation . 24
4.2.6.2.5 Specification 4: Fault conditions . 25
4.2.6.2.6 Conformance tests . 25
4.2.7 Receive antenna off-axis gain pattern . 25
4.2.7.1 Justification . 25
4.2.7.2 Specification. 25
4.2.7.3 Conformance tests . 26
4.2.8 Blocking performance . 26
4.2.8.1 Justification . 26
4.2.8.2 Specification. 26
4.2.8.3 Conformance tests . 26
4.2.9 Adjacent Signal Selectivity . 26
4.2.9.1 Justification . 26
4.2.9.2 Specification. 26
4.2.9.3 Conformance tests . 27
5 Testing for compliance with technical requirements . 27
5.1 Environmental conditions for testing . 27
5.2 Essential radio test suites . 27
6 Test methods . 27
6.0 General . 27
6.1 Spurious radiation. 28
6.1.1 Test method . 28
6.1.1.0 Introduction . 28
6.1.1.1 Up to 1 000 MHz (see clause 4.2.2.2, table 2) . 29
6.1.1.1.1 Test site. 29
6.1.1.1.2 Measuring receivers . 29
6.1.1.1.3 Procedure . 29
6.1.1.2 Above 1 000 MHz (see clause 4.2.2.2, tables 3 and 4) . 29
6.1.1.2.0 General . 29
6.1.1.2.1 Identification of the significant frequencies of spurious radiation . 30
6.1.1.2.2 Measurement of radiated power levels of identified spurious radiation . 30
6.2 On-axis spurious radiation . 31
6.2.1 Test method . 31
6.2.1.1 Test site . 31
6.2.1.2 Method of measurement . 31
6.2.1.2.1 General . 31
6.2.1.2.2 Method of measurement at the antenna flange . 32
6.2.1.2.3 Method of measurement with a test antenna . 32
6.3 Off-axis EIRP emissions density in the nominated bandwidth . 33
6.3.1 General . 33
6.3.2 rms antenna pointing accuracy. 34
6.3.2.1 Method of measurement . 34
6.3.3 Measurement of the off-axis EIRP without the antenna . 35
6.3.3.1 Transmitter output power density . 35
6.3.3.1.0 General . 35
6.3.3.1.1 Method of measurement . 35
6.3.3.2 Antenna transmit gain . 35
6.3.3.2.1 General . 35
6.3.3.2.2 Test site. 35
6.3.3.2.3 Method of measurement . 36
ETSI
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5 ETSI EN 302 186 V2.1.1 (2016-05)
6.3.3.3 Antenna transmit radiation patterns . 37
6.3.3.3.1 General . 37
6.3.3.3.2 Test site. 37
6.3.3.3.3 Method of measurement . 37
6.3.3.4 Computation of results . 38
6.3.4 Measurement of the off-axis EIRP with the antenna . 38
6.3.4.1 General . 38
6.3.4.2 Maximum EIRP density per 40 kHz ratio relative to the EIRP . 38
6.3.4.2.0 General . 38
6.3.4.2.1 Method of measurement . 38
6.3.4.3 Maximum on-axis EIRP . 39
6.3.4.3.1 General . 39
6.3.4.3.2 Test site. 39
6.3.4.3.3 Method of measurement . 39
6.3.4.4 Antenna transmit radiation patterns . 41
6.3.4.4.1 General . 41
6.3.4.4.2 Test site. 41
6.3.4.4.3 Method of measurement . 41
6.3.4.5 Computation of results . 42
6.4 Power Flux Density Test . 42
6.4.1 General . 42
6.4.2 Verification of specification 1: Mode of PFD limitation . 43
6.4.3 Verification of specification 2: Location where to limit the PFD . 43
6.4.4 Verification of specification 3: PFD limitatio n . 43
6.4.4.1 Measurement of the antenna radiation pattern below the aircraft fuselage . 43
6.4.4.1.1 General . 43
6.4.4.1.2 Test site. 43
6.4.4.1.3 Test method procedure . 43
6.4.4.2 Measurement of on-axis EIRP as a function of altitude . 44
6.4.4.2.1 General . 44
6.4.4.2.2 Test site. 45
6.4.4.2.3 Method of measurement with a test antenna . 45
6.4.4.3 Computation of the power flux density at the surface of the Earth . 46
6.4.5 Verification of specification 4: Fault conditions . 46
6.4.5.1 Test Arrangement . 46
6.4.5.2 Test method . 46
6.5 Control and monitoring . 47
6.5.0 General . 47
6.5.1 Test arrangement . 47
6.5.2 Processor monitoring . 48
6.5.2.1 Test method . 48
6.5.3 Transmit subsystem monitoring . 48
6.5.3.1 Test method . 48
6.5.4 Power-on/Reset . 49
6.5.4.1 Test method . 49
6.5.5 Control Channel (CC) reception . 49
6.5.5.1 Test method . 49
6.5.6 Network control commands . 50
6.5.6.1 Test method . 50
6.5.7 Initial burst transmission . 51
6.5.7.1 Test method . 51
6.6 Receive antenna off-axis gain pattern . 51
6.6.1 Test method . 51
6.6.1.1 Test site . 51
6.6.1.2 Method of measurement . 52
6.6.1.3 Computation . 52
6.7 Blocking performance . 52
6.7.1 Test method .
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