A Technical Comparison of Three Low Earth Orbit Satellite Constellation Systems to Provide Global Broadband
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1 A Technical Comparison of Three Low Earth Orbit Satellite Constellation Systems to Provide Global Broadband Inigo del Portillo Bruce G. Cameron, Edward F. Crawley Massachusetts Institute of Technology October 1st th International Astronautical Congress 2018 Bremen, Germany IAC-18-B
2 In the last 3 years there has been a new wave of proposals of LEO mega-constellations to provide broadband. (11 proposals) Motivation This paper compares the technical aspects of three of these systems as described in their FCC application filings: OneWeb, SpaceX, and Telesat Moreover, we analyze ground segment requirements and estimate the total system forward capacity (sellable capacity) for each of the systems. 2
3 Description: OneWeb s Ku&Ka-band System System characteristics 720 satellites in 18 polar planes at 1, º (40 satellites per plane) User Ku-band, gateway Bent pipe architecture No crosslinks Compact satellites 145 kg. Target first launch Q4 18, Q1 19 (21 Soyuz rockets) Beginning of service 2019 Figure 1.- OneWeb 720 satellites constellation Image credit: OneWeb Description Comparison Methodology Results Conclusions 3
4 Description: SpaceX s Ku&Ka-band System System characteristics 4,425 Satellites in 83 planes. Inclined orbits + polar orbits. User Ku-band, gateway Optical crosslinks between satellites Digital payload with beam steering and shaping capabilities Medium size satellites 435 kg, in house designed. Target first launch 2019 (~170 Falcon 9 launches for full constellation deployment) Beginning of service 2020 Figure 2.- SpaceX 4,425 satellites constellation Image credit: SpaceX Description Comparison Methodology Results Conclusions 4
5 Description: Telesat s Ka-band System System characteristics 117 Satellites in 12 planes: Polar: 6 planes x 12 satellites at 1, º Inclined: 5 planes x 10 satellites at 1, User and gateway Optical crosslinks between satellites Digital payload: Beamforming: steering and shaping capabilities for at least 16 beams. Demodulation + modulation + IP-Routing Launch 2021 Beginning of service 2022 External design and manufacturing. Figure 3.- Telesat 117 satellites constellation Description Comparison Methodology Results Conclusions 5
6 Satellites in line of sight and beam characteristics Great differences in the number of satellites within line of sight for different latitudes between constellations. Telesat and SpaceX concentrate their satellites within the ±60 latitude band by using inclined and polar orbits. Significant differences in beam footprint and field-of-view areas. SpaceX and Telesat have steerable and shapeable user beams. One web has fixed beams. Description Comparison Methodology Results Conclusions 6
7 Frequency allocations OneWeb and SpaceX use Ku-band for user links. Single polarization, RHCP, and Ka-band for gateway links. Telesat shares the Ka-band spectrum between user and gateways links. Potential interferences during in-line events between: OneWeb and SpaceX user links. Telesat user links and OneWeb and SpaceX feeder links Key GSO TFS FSS MSS BSS Downlinks Uplinks Geostationary satellite orbit Terrestrial fixed service Fixed satellite service Mobile satellite service Broadcast satellite service OneWeb SpaceX Telesat Gateway-links User-links Gateway-links User-links Gateway-links User-links TT&C-links TT&C-links TT&C-links MSS FL Mobile satellite service feeder links LMDS Local multipoint distribution service NGSO Non-geostationary satellite orbit Description Comparison Methodology Results Conclusions 7
8 Methodology: Model overview Link parameters Constellation orbital info. Atmospheric models ITU Link Budget Orbital Dynamics Total throughput estimation Statistical model Table 8. Average and maximum potential data-rate per satellite (author s estimation) Parameter Telesat OneWeb SpaceX Avg. Data-rate Gbps Max. Data-rate Gbps # Active GW antennas Limiting factor GW uplink User downlink GW uplink - Candidate GS locations Demand map Ground segment optimization Genetic Algorithm Optimal ground segment Description Comparison Methodology Results Conclusions 8
9 Results: Throughput estimation Telesat OneWeb SpaceX OneWeb + ISL Telesat: Maximum throughput is 2.66 Tbps and 42 ground stations are required to achieve it. SpaceX: Maximum throughput of 23.7 Tbps with > 100 GS. OneWeb Maximum throughput is 1.56 Tbps, and need 71 ground station to achieve it. Description Comparison Methodology Results Conclusions 9
10 Results: Summary of values Telesat: Telesat is the most efficient system in terms of average Gbps/satellite, with more than 4x SpaceX and 10x OneWeb. SpaceX: SpaceX limiting factor will be the ground segment, as they need to deploy a very large number of ground stations and gateways to operate at full power. OneWeb For OneWeb the space segment will be the limiting factor (user links data-rate). Telesat OneWeb SpaceX Num. satellites ,425 - Max. total system FWD capacity Tbps Number of ground locations for max. FWD capacity Number of gateway antennas for max FWD ~3,500 - capacity Required number of gateways per ground station Average data-rate per satellite (real) Gbps Max. data-rate per satellite Gbps Satellite efficiency % Description Comparison Methodology Results Conclusions 10
11 Conclusions Estimated maximum system throughputs in the forward direction: OneWeb s 1.56 Tbps with 71 ground stations (720 satellites) Telesat 2.66 Tbps with 40 ground stations (117 satellites) SpaceX 23.7 Tbps with 123 ground stations (4,425 satellites) The most effective system in terms of Gbps/satellite is Telesat (22.7 Gbps/sat), thanks to: Low number of high capacity satellites, low elevation angles to user links, use of ISL and digital payloads, and use of two active gateway antennas. SpaceX constellation will require an extremely large ground segment with hundreds of ground stations and ~3,500 gateway antennas to operate at maximum throughput. OneWeb s constellation could significantly reduce their ground segment if they had used inter-satellite links (even at moderate data-rates ~5 Gbps). Description Comparison Methodology Results Conclusions 11
12 THANK YOU! Contact
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