1、 Recommendation ITU-R SA.1019-1 (07/2017) Frequency bands and transmission directions for data relay satellite networks/systems SA Series Space applications and meteorology ii Rec. ITU-R SA.1019-1 Foreword The role of the Radiocommunication Sector is to ensure the rational, equitable, efficient and
2、economical use of the radio-frequency spectrum by all radiocommunication services, including satellite services, and carry out studies without limit of frequency range on the basis of which Recommendations are adopted. The regulatory and policy functions of the Radiocommunication Sector are performe
3、d by World and Regional Radiocommunication Conferences and Radiocommunication Assemblies supported by Study Groups. Policy on Intellectual Property Right (IPR) ITU-R policy on IPR is described in the Common Patent Policy for ITU-T/ITU-R/ISO/IEC referenced in Annex 1 of Resolution ITU-R 1. Forms to b
4、e used for the submission of patent statements and licensing declarations by patent holders are available from http:/www.itu.int/ITU-R/go/patents/en where the Guidelines for Implementation of the Common Patent Policy for ITU-T/ITU-R/ISO/IEC and the ITU-R patent information database can also be found
5、. Series of ITU-R Recommendations (Also available online at http:/www.itu.int/publ/R-REC/en) Series Title BO Satellite delivery BR Recording for production, archival and play-out; film for television BS Broadcasting service (sound) BT Broadcasting service (television) F Fixed service M Mobile, radio
6、determination, amateur and related satellite services P Radiowave propagation RA Radio astronomy RS Remote sensing systems S Fixed-satellite service SA Space applications and meteorology SF Frequency sharing and coordination between fixed-satellite and fixed service systems SM Spectrum management SN
7、G Satellite news gathering TF Time signals and frequency standards emissions V Vocabulary and related subjects Note: This ITU-R Recommendation was approved in English under the procedure detailed in Resolution ITU-R 1. Electronic Publication Geneva, 2017 ITU 2017 All rights reserved. No part of this
8、 publication may be reproduced, by any means whatsoever, without written permission of ITU. Rec. ITU-R SA.1019-1 1 RECOMMENDATION ITU-R SA.1019-1 Frequency bands and transmission directions for data relay satellite networks/systems (Question ITU-R 118/7) (1994-2017) Scope This Recommendation provide
9、s the recommended frequency bands and the transmission directions for data relay satellite networks/systems. Keywords DRS, space-to-Earth, Earth-to-space, space-to-space, forward feeder link, return feeder link Related ITU-R Recommendations and Reports Recommendations ITU-R SA.510, ITU-R SA.1018, IT
10、U-R SA.1155, ITU-R SA.1274, ITU-R SA.1275, ITU-R SA.1276, ITU-R SA.1414. The ITU Radiocommunication Assembly, considering a) that data relay satellite networks/systems are in operation or are planned corresponding to the Hypothetical Reference System for Data Relay Satellite (DRS) Systems of Recomme
11、ndation ITU-R SA.1018; b) that these DRS systems support links with widely different characteristics as described in the Annex; c) that some DRS user spacecraft require links of low data rate (up to about 6 Mbit/s) which require modest bandwidths which can be most economically implemented, using low
12、-power transmitters, simple wide-beam antennas without complex pointing mechanisms and robust receivers, in frequency bands for DRS inter-orbit links below 3 GHz; d) that some DRS user spacecraft require links from wide-beam or omnidirectional antennas (in particular to support contingency links) in
13、 cases where the attitude of the user spacecraft and the direction of the DRS is not accurately known, thus requiring the use of frequency bands for DRS inter-orbit links below 3 GHz; e) that some DRS user spacecraft require links of medium to high data rates (from about 6 Mbit/s up to more than 600
14、 Mbit/s) thus requiring the use of frequency bands for DRS inter-orbit links above 10 GHz; f) that the frequency bands available and suitable for DRS inter-orbit links are limited; g) that the forward and return feeder links of data relay satellites could use bands allocated to the fixed-satellite s
15、ervice; h) that the normal-mode operations of data relay satellites should use their own forward and return feeder link frequency bands; 2 Rec. ITU-R SA.1019-1 i) that launch, early-orbit-phase and emergency operations of data relay satellites require the use of wide-beam or omnidirectional antennas
16、, which require the use of frequency bands below 3 GHz; j) that the choice of common frequency bands for different data relay satellite systems permits the consideration of interoperability between user spacecraft designed to use one DRS system and data relay satellites of another DRS system; k) tha
17、t Recommendation ITU-R SA.1414 provides parameters including frequencies for DRS systems worldwide to be used as guidance for deriving sharing criteria and coordination thresholds, recommends 1 that the inter-orbit links for DRS user spacecraft requiring low data rates using wide-beam or omnidirecti
18、onal antennas use assignments within the allocated bands: 1.1 2 025-2 110 MHz band for the forward inter-orbit link; 1.2 2 200-2 290 MHz band for the return inter-orbit link; 2 that the inter-orbit links for DRS user spacecraft requiring medium data rates consider assignments within the allocated ba
19、nds, subject to the limitations of a secondary allocation: 2.1 13.4-14.3 GHz band for the forward inter-orbit link; 2.2 14.5-15.35 GHz band for the return inter-orbit link; 3 that the inter-orbit links for DRS user spacecraft requiring medium to high data rates use assignments within the allocated b
20、ands: 3.1 22.55-23.55 GHz band for the forward inter-orbit link; 3.2 25.25-27.50 GHz band for the return inter-orbit link; 4 that the launch, early-orbit-phase and emergency operations of a DRS use the 2 025-2 110 MHz and 2 200-2 290 MHz bands; 5 that the frequency bands shown in Table 1 below shoul
21、d be used for DRS system reference architecture links taking into account the information available in Recommendation ITU-R SA.1414. TABLE 1 DRS System frequency bands and directions of transmission Application Direction of transmission Frequency Inter-orbit link Low data rate (300 Mb/s) requirement
22、 Forward 22.55-23.55 GHz Return 25.25-27.5 GHz DRS satellite feeder links Launch, early orbit, and contingency command and telemetry Uplink 2 025-2 110 MHz Downlink 2 200-2 290 MHz DRS satellite feeder links Low and medium data rate requirement Forward feeder link (Uplink) 14.5-15.35 GHz 12.75-13.25
23、 GHz 14.5-14.75 GHz High data rate requirement 27.5-31 GHz Low and medium data rate requirement Return feeder link (Downlink) 13.4-13.75 GHz 13.75-14.3 GHz 10.7-11.7 GHz 12.5-12.75 GHz 13.4-13.65 GHz High data rate requirement 17.7-21.2 GHz 25.5-27 GHz (see Note 1) NOTE 1 In the frequency band 25.5-
24、27 GHz, the return DRS-to-Earth feeder link carries only signals in the space research and Earth exploration-satellite services. Annex 1 Introduction Communication between the ground and low-Earth orbiting spacecraft and launch vehicles used for space research, Earth exploration and other purposes i
25、s essential. Such communications may be required to be continuous or near-continuous, or may be required while the spacecraft are passing over specific points on the Earths surface. Land based earth stations have only a limited visibility and existing stations are only capable of covering a portion
26、of any low-Earth orbit. Moreover, it is not economically or practically feasible to extend networks of land-based stations to provide full or more complete coverage of the low-Earth orbits. In contrast, a data relay satellite (DRS) system including one or more DRS satellites in geostationary orbit h
27、as substantially larger visibility of the low-Earth orbits used by these satellites than existing land-based earth stations, and can therefore provide significantly enhanced coverage. A single DRS satellite in geostationary orbit can provide communications between an earth station and a low-orbiting
28、 spacecraft for more than one-half of its orbit. Two such DRSs, suitably located in geostationary orbit, with a wide separation angle, can provide communications between two co-located earth stations and a low-orbiting spacecraft almost continuously, with the exception only of a zone of exclusion (Z
29、OE), above the part of the Earth opposite to these earth stations. Moreover; two such DRSs, suitably placed in geostationary orbit, can provide fully-continuous coverage between two separate earth stations and a low-orbiting spacecraft. A DRS system can also serve 4 Rec. ITU-R SA.1019-1 additional e
30、arth stations, either both transmitting and receiving or only receiving signals from user spacecraft. 2 Description of the data relay satellite network/system A DRS consists of one or more DRS spacecraft in geostationary orbit and one or more DRS earth stations. The system relays information between
31、 the earth station(s) and DRS users, which can include low-Earth orbiting spacecraft, launch vehicles, and even ground based or aeronautical platforms. A DRS system must be capable of supporting at least four distinct links: an Earth-to-space link in the forward direction, from the earth station to
32、the data relay satellite (known as the uplink or the forward feeder link); a space-to-space link in the forward direction, from the data relay satellite to the low orbit spacecraft (known as the forward inter-orbit link); a space-to-space link in the return direction, from the low orbit spacecraft t
33、o the data relay satellite (known as the return inter-orbit link); and a space-to-Earth link in the return direction, from the data relay satellite to the earth station (known as the downlink or the return feeder link). In the forward direction, the input to the DRS system reference architecture cor
34、responds to the baseband data provided at the input of the DRS earth station modulator which modulates the feeder uplink carrier. This baseband data typically consists of command data and (in the case of manned missions) voice and video information. It is provided to the DRS earth station over an ex
35、ternal interface (landline communication, RF terrestrial link, etc.) by the Mission Operations Control Center (MOCC) responsible for the user spacecraft. Note that the MOCC and the external interface to the DRS earth station are not part of the reference architecture. For the case of a demodulating
36、receiver on board the user spacecraft, the output of the DRS system reference architecture in the forward direction corresponds to the output of the demodulator on board the user satellite. For the case of a repeater on board the user spacecraft, it corresponds to the output of the earth station dem
37、odulator receiving the return feeder link signal. In the return direction, the input to the DRS reference architecture corresponds to the input of the user spacecraft modulator carrying out the translation from the baseband to the radio-frequency carrier. This baseband data typically consists of rea
38、l-time and/or recorded scientific data, or for manned missions, voice and video information. The output of the reference architecture corresponds to the output of the earth station demodulator carrying out the reverse operation. 3 Frequency bands and transmission directions Each of the DRS system ar
39、chitecture links defined in 2 must necessarily transmit in a separate frequency band, with a guard band between the signals transmitted from and those received by the data relay satellite. In determination of the frequency bands for these links, there are many factors to consider. These include the
40、allocation status and bandwidth of available bands, antenna beam width and propagation characteristics. It is noted that the choice of a common frequency band for different data relay satellite networks/systems requires the consideration of interoperability between user spacecraft designed to use on
41、e DRS system and data relay satellites of another DRS system. For the forward and return inter-orbit links, the characteristics of the wide variety of different types of DRS users dictate the use of multiple bands. Some DRS user spacecraft require links of low data rate (up to about 6 Mbit/s) which
42、require modest bandwidths, and can be most economically implemented using low-power transmitters and simple wide-beam antennas without complex Rec. ITU-R SA.1019-1 5 pointing mechanisms along with robust receivers. Some other DRS user spacecraft require links from wide-beam or omnidirectional antenn
43、as (in particular to support contingency links) in cases where the attitude of the user spacecraft and the direction of the DRS is not accurately known. For these classes of DRS users, the use of inter-orbit link frequencies below 3 GHz is ideal. Other DRS user spacecraft require links of medium to
44、high data rates (from about 6 Mbit/s up to 600 Mbit/s) and therefore require the use of frequency bands for DRS inter-orbit links above 10 GHz. For the forward and return feeder links, it is noted that DRS systems could use either frequency bands allocated for the fixed satellite service or those al
45、located for the space research service and that there are a number of bands allocated with sufficient bandwidth to support the data transfer requirements of the inter-orbit links as described above. For nominal DRS satellite operations, these bands are also appropriate for DRS spacecraft command and telemetry. However for the launch, early-orbit-phase and emergency operations of DRS satellites, where omnidirectional antennas may be needed, a frequency band below 3 GHz is preferred.
