Satellite Earth Stations and Systems (SES); Aircraft Earth Stations (AES) operating under the Aeronautical Mobile Satellite Service (AMSS)/Mobile Satellite Service (MSS) and/or the Aeronautical Mobile Satellite on Route Service (AMS(R)S)/Mobile Satellite Service (MSS)

REN/SES-00073

Satelitske zemeljske postaje in sistemi (SES) – Letalske zemeljske postaje (AES), ki obratujejo v letalski mobilni satelitski storitvi (AMSS) in mobilni satelitski storitvi (MSS) oziroma v letalski mobilni satelitski storitvi na poti (AMS(R)S) in mobilni satelitski storitvi (MSS)

General Information

Status
Published
Publication Date
18-Aug-2004
Current Stage
12 - Completion
Due Date
27-Aug-2004
Completion Date
19-Aug-2004
Standard
EN 301 473 V1.3.1:2006
English language
66 pages
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Standards Content (Sample)


SLOVENSKI STANDARD
01-februar-2006
Satelitske zemeljske postaje in sistemi (SES) – Letalske zemeljske postaje (AES),
ki obratujejo v letalski mobilni satelitski storitvi (AMSS) in mobilni satelitski
storitvi (MSS) oziroma v letalski mobilni satelitski storitvi na poti (AMS(R)S) in
mobilni satelitski storitvi (MSS)
Satellite Earth Stations and Systems (SES); Aircraft Earth Stations (AES) operating
under the Aeronautical Mobile Satellite Service (AMSS)/Mobile Satellite Service (MSS)
and/or the Aeronautical Mobile Satellite on Route Service (AMS(R)S)/Mobile Satellite
Service (MSS)
Ta slovenski standard je istoveten z: EN 301 473 Version 1.3.1
ICS:
33.060.30 Radiorelejni in fiksni satelitski Radio relay and fixed satellite
komunikacijski sistemi communications systems
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

ETSI EN 301 473 V1.3.1 (2004-08)
European Standard (Telecommunications series)

Satellite Earth Stations and Systems (SES);
Aircraft Earth Stations (AES) operating under the
Aeronautical Mobile Satellite Service (AMSS)/
Mobile Satellite Service (MSS) and/or the
Aeronautical Mobile Satellite on Route Service (AMS(R)S)/
Mobile Satellite Service (MSS)

2 ETSI EN 301 473 V1.3.1 (2004-08)

Reference
REN/SES-00073
Keywords
AMSS, aeronautical, earth station, mobile, MSS,
satellite
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ETSI
3 ETSI EN 301 473 V1.3.1 (2004-08)
Contents
Intellectual Property Rights.8
Foreword.8
Introduction .8
1 Scope.9
2 References.9
3 Definitions and abbreviations.10
3.1 Definitions.10
3.2 Abbreviations.11
4 General.12
4.1 Presentation of equipment for testing purposes.12
4.2 Aircraft earth stations .12
4.3 Description of equipment .13
5 Requirements for AES transmitting in the band 1 610 MHz to 1 626,5 MHz .13
5.1 Unwanted emissions limits outside the band 1 610 MHz to 1 626,5 MHz and the band 1 626,5 MHz to
1 628,5 MHz (carrier-on) .13
5.1.1 Purpose.13
5.1.2 Conformance requirements.14
5.1.3 Method of test .14
5.1.4 Peak measurement.15
5.1.5 Average measurement.15
5.1.6 Test requirements.15
5.2 Unwanted emissions limits within the band 1 610 MHz to 1 626,5 MHz and the band 1 626,5 MHz to
1 628,5 MHz (carrier-on) .15
5.2.1 Purpose.15
5.2.2 Conformance requirements.16
5.2.3 Method of test .17
5.2.4 Measurement method.17
5.2.5 Test requirements.18
5.3 EIRP density limits within the operational band .18
5.3.1 Purpose.18
5.3.2 Conformance requirements.18
5.3.3 Method of test .18
5.3.4 Peak Limit Test.19
5.3.5 Mean Limit Test .19
5.3.6 Test requirements.19
5.4 Unwanted emissions limits (carrier-off).20
5.4.1 Purpose.20
5.4.2 Conformance requirements.20
5.4.3 Method of test .20
5.4.4 Peak measurement.20
5.4.5 Average measurement.21
5.4.6 Test requirements.21
5.5 AES Control and Monitoring Functions (CMF).21
5.5.1 Special test equipment .21
5.5.2 Self-monitoring functions.21
5.5.2.1 Processor monitoring.21
5.5.2.1.1 Purpose.21
5.5.2.1.2 Conformance requirements.21
5.5.2.1.3 Method of test.22
5.5.2.2 Transmit frequency generation sub-system monitoring .22
5.5.2.2.1 Purpose.22
5.5.2.2.2 Conformance requirements.22
5.5.2.2.3 Method of test.22
ETSI
4 ETSI EN 301 473 V1.3.1 (2004-08)
5.5.3 Network control authorization and reception.22
5.5.3.1 Network control authorization .22
5.5.3.1.1 Purpose.22
5.5.3.1.2 Conformance requirements.22
5.5.3.1.3 Method of test.22
5.5.3.1.4 Test procedure.23
5.5.3.1.5 Test requirement.23
5.5.3.2 Network control reception transmit frequency control.23
5.5.3.2.1 Purpose.23
5.5.3.2.2 Conformance requirements.23
5.5.3.2.3 Method of test.23
5.5.3.2.4 Test procedure.24
5.5.3.2.5 Test requirement.24
5.6 Equipment identity.24
5.6.1 Purpose.24
5.6.2 Conformance requirements.24
5.6.3 Method of test .24
5.6.4 Test procedure.25
5.6.5 Test requirements.25
6 Requirements for AES transmitting in the band 1 626,5 MHz to 1 660,5 MHz .25
6.1 Unwanted emissions limits outside the band 1 626,5 MHz to 1 660,5 MHz and the band 1 660,5 MHz to
1 662,5 MHz.25
6.1.1 Purpose.25
6.1.2 Conformance requirements.25
6.1.3 Testing for carrier on state .28
6.1.3.1 Method of test .28
6.1.3.2 Measurement method.29
6.1.3.3 Test requirements.29
6.1.4 Testing for carrier off state .29
6.1.4.1 Method of test .29
6.1.4.2 Peak measurement method.30
6.1.4.3 Average measurement.30
6.1.4.4 Test requirements.30
6.2 Unwanted emissions limits within the band 1 626,5 MHz to 1 660,5 MHz and the band 1 660,5 MHz to
1 662,5 MHz.30
6.2.1 Purpose.30
6.2.2 Conformance requirements.31
6.2.2.1 General.31
6.2.2.2 Specification 1: Carrier-on state.31
6.2.2.3 Specification 2: Carrier-off state.32
6.2.3 Testing for carrier on state .32
6.2.3.1 Method of test .32
6.2.3.2 Measurement method.32
6.2.3.3 Test requirements.33
6.2.4 Testing for carrier off state .33
6.2.4.1 Method of test .33
6.2.4.2 Peak measurement method.33
6.2.4.3 Average measurement.33
6.2.4.4 Test requirements.34
6.3 AES Control and Monitoring Functions (CMF).34
6.3.1 Special test equipment .34
6.3.2 Self-monitoring functions.34
6.3.2.1 Processor monitoring.34
6.3.2.1.1 Purpose.34
6.3.2.1.2 Conformance requirements.34
6.3.2.1.3 Method of test.34
6.3.2.2 Transmit frequency generation sub-system monitoring .34
6.3.2.2.1 Purpose.34
6.3.2.2.2 Conformance requirements.34
6.3.2.2.3 Method of test.35
6.3.3 Network control authorization and reception.35
ETSI
5 ETSI EN 301 473 V1.3.1 (2004-08)
6.3.3.1 Network control authorization .35
6.3.3.1.1 Purpose.35
6.3.3.1.2 Conformance requirements.35
6.3.3.1.3 Method of test.35
6.3.3.1.4 Test procedure.35
6.3.3.1.5 Test requirement.36
6.3.3.2 Network control reception transmit frequency control.36
6.3.3.2.1 Purpose.36
6.3.3.2.2 Conformance requirements.36
6.3.3.2.3 Method of test.36
6.3.3.2.4 Test procedure.36
6.3.3.2.5 Test requirement.37
6.4 Equipment identity.37
6.4.1 Purpose.37
6.4.2 Conformance requirements.37
6.4.3 Method of test .37
6.4.4 Test procedure.37
6.4.5 Test requirements.37
7 Requirements for AES transmitting in the band 1 980 MHz to 2 010 MHz .38
7.1 Unwanted emissions limits outside the band 1 980,1 MHz to 2 009,9 MHz (carrier-on) .38
7.1.1 Purpose.38
7.1.2 Conformance requirements.38
7.1.3 Method of test .39
7.1.4 Peak measurement.39
7.1.5 Average measurement.39
7.1.6 Test requirements.40
7.2 Unwanted emissions limits within the bands 1 980,1 MHz to 2 009,9 MHz, 1 978,1 MHz to
1 980,1 MHz and 2 009,9 MHz to 2 011,9 MHz (carrier-on).40
7.2.1 Purpose.40
7.2.2 Conformance requirements.40
7.2.3 Method of test .41
7.2.4 Measurement method.41
7.2.5 Test requirements.42
7.3 Unwanted emissions limits (carrier-off).42
7.3.1 Purpose.42
7.3.2 Conformance requirements.42
7.3.3 Method of test .42
7.3.4 Peak measurement.43
7.3.5 Average measurement.43
7.3.6 Test requirements.43
7.4 AES Control and Monitoring Functions (CMF).43
7.4.1 Special test equipment .43
7.4.2 Self-monitoring functions.44
7.4.2.1 Processor monitoring.44
7.4.2.1.1 Purpose.44
7.4.2.1.2 Conformance requirements.44
7.4.2.1.3 Method of test.44
7.4.2.2 Transmit frequency generation sub-system monitoring .44
7.4.2.2.1 Purpose.44
7.4.2.2.2 Conformance requirements.44
7.4.2.2.3 Method of test.44
7.4.3 Network control authorization and reception.44
7.4.3.1 Network control authorization .44
7.4.3.1.1 Purpose.44
7.4.3.1.2 Conformance requirements.45
7.4.3.1.3 Method of test.45
7.4.3.1.4 Test procedure.45
7.4.3.1.5 Test requirement.45
7.4.3.2 Network control reception.46
7.4.3.2.1 Transmit frequency control .46
7.5 Equipment identity.47
ETSI
6 ETSI EN 301 473 V1.3.1 (2004-08)
7.5.1 Purpose.47
7.5.2 Conformance requirements.47
7.5.3 Method of test .47
7.5.4 Test procedure.47
7.5.5 Test requirements.47
8 Protection of the global navigation satellite service operating in the band 1 559 MHz to
1 610 MHz.47
8.1 1 559 MHz to 1 605 MHz .47
8.1.1 Purpose.47
8.1.2 Conformance requirements.48
8.2 1 605 MHz to 1 610 MHz .48
8.2.1 Purpose.48
8.2.2 Conformance requirements.48
8.3 Method of test.48
8.4 Average measurement.49
8.5 Test requirements.49
9 Protection of the radio astronomy services operating in the band 1 610,6 MHz to 1 613,8 MHz
and in the band 1 660 MHz to 1 670 MHz.49
9.1 Purpose.49
9.2 Conformance requirements.50
9.2.1 Alternative 1.50
9.2.2 Alternative 2.50
9.3 Method of test - unwanted emissions (alternative 1).51
9.4 Test procedure - unwanted emissions (alternative 1) .51
9.5 Test requirement - unwanted emissions (alternative 1).51
9.6 Method of test - CMF function (alternative 2) .52
9.7 Test procedure- CMF function (alternative 2).52
9.8 Test requirement- CMF function (alternative 2) .52
Annex A (normative): General test requirements.53
A.1 AES test modes .53
A.2 Special Test Equipment.53
A.2.1 STE description.53
A.2.2 Use of STE for control and monitoring functions tests .54
A.2.3 Test modulating signal .54
A.3 Laboratory Test Equipment.55
A.4 Interpretation of the measurement results .55
A.5 Test report.55
Annex B (normative): Environmental conditions .56
B.1 General.56
B.2 Environmental conformance requirements.56
B.3 Environmental test conditions.56
Annex C (normative): Arrangements for measurement of emissions from AES.57
C.1 General.57
C.2 Carrier-on emissions.57
C.2.1 Equipment required.57
C.2.2 Equipment arrangement.58
C.2.3 Emissions from 4 GHz to 18 GHz.58
C.2.4 Emissions from 10 kHz to 4 GHz.58
C.3 Carrier-off emissions.59
C.3.1 Equipment required.59
C.3.2 Equipment arrangement.59
ETSI
7 ETSI EN 301 473 V1.3.1 (2004-08)
C.3.3 Carrier-off emissions from 4 GHz to 18 GHz .59
C.3.4 Carrier-off emissions from 10 kHz to 4 GHz .60
Annex D (informative): Explanation of nominated bandwidth.61
D.1 Introduction.61
D.2 Interpretation of Parameters [Bn, f , a, b].61
c
D.3 Choice of nominated bandwidth.61
D.4 Maximum value for nominated bandwidth .63
Annex E (informative): Bibliography.65
History .66

ETSI
8 ETSI EN 301 473 V1.3.1 (2004-08)
Intellectual Property Rights
IPRs essential or potentially essential to the present document may have been declared to ETSI. The information
pertaining to these essential IPRs, if any, is publicly available for ETSI members and non-members, and can be found
in ETSI SR 000 314: "Intellectual Property Rights (IPRs); Essential, or potentially Essential, IPRs notified to ETSI in
respect of ETSI standards", which is available from the ETSI Secretariat. Latest updates are available on the ETSI Web
server (http://webapp.etsi.org/IPR/home.asp).
Pursuant to the ETSI IPR Policy, no investigation, including IPR searches, has been carried out by ETSI. No guarantee
can be given as to the existence of other IPRs not referenced in ETSI SR 000 314 (or the updates on the ETSI Web
server) which are, or may be, or may become, essential to the present document.
Foreword
This European Standard (Telecommunications series) has been produced by ETSI Technical Committee Satellite Earth
Stations and Systems (SES).
National transposition dates
Date of adoption of this EN: 13 August 2004
Date of latest announcement of this EN (doa): 30 November 2004
Date of latest publication of new National Standard
or endorsement of this EN (dop/e): 31 May 2005
Date of withdrawal of any conflicting National Standard (dow): 31 May 2005

Introduction
An AES to be effectively used on board an aircraft will also be subject to airworthiness approval. This approval will
refer to additional requirements (e.g. ISO 7137 equivalent to EUROCAE ED-14D and RTCA DO-160D [1]).
Foreseeable evolution of the GNSS (i.e. Galileo or GPS L5) would result in the coming years in specific requirements
to protect the use of the GNSS signals on board aircraft. Therefore these new GNSS frequency bands may require
different protection than currently stated in the present document.
ETSI
9 ETSI EN 301 473 V1.3.1 (2004-08)
1 Scope
The present document specifies certain minimum technical performance requirements of Aircraft Earth Station (AES)
equipment with both transmit and receive capabilities for operation in the Aeronautical Mobile Satellite Service
(AMSS)/Mobile Satellite Service (MSS), and/or in the Aeronautical Mobile Satellite on Route Service
(AMS(R)S)/Mobile Satellite Service (MSS), in the frequency bands given in table 1.
Table 1: Aeronautical Mobile Satellite Service (AMSS)/Mobile Satellite Service (MSS),
and/or Aeronautical Mobile Satellite on Route Service (AMS(R)S)/
Mobile Satellite Service (MSS) frequency bands
AMSS/MSS and/or AMS(R)S/MSS frequency bands
AES transmit 1 610 MHz to 1 626,5 MHz
AES receive 1 613,8 MHz to 1 626,5 MHz
AES receive 2 483,5 MHz to 2 500 MHz
AES transmit 1 626,5 MHz to 1 660,5 MHz
AES receive 1 525 MHz to 1 559 MHz
AES transmit 1 980 MHz to 2 010 MHz
AES receive 2 170 MHz to 2 200 MHz

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 Facilities (NCF) for its supporting satellite network.
NOTE: The requirements for Network Control Facilities (NCF) for S-PCN MES transmitting in the 1 610 MHz to
1 626,5 MHz band or the 1 980 MHz to 2 010 MHz band are contained in ETS 300 735 [4]; these
requirements are also applicable to AES transmitting in those bands.
An AES may be subject to additional or alternative requirements in other standards depending on its functionality, in
particular if it supports a service which is considered a justified case for regulation of terminal equipment interworking
via the public telecommunications network. An AES will also be subject to additional airworthiness certification
requirements.
2 References
The following documents contain provisions which, through reference in this text, constitute provisions of the present
document.
• References are either specific (identified by date of publication and/or edition number or version number) or
non-specific.
• For a specific reference, subsequent revisions do not apply.
• For a non-specific reference, the latest version applies.
Referenced documents which are not found to be publicly available in the ex
...

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