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USING THE NEW L BAND MSS ALLOCATIONS Study Group 8 Seminar on Tomorrows Technological Innovations Ge

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Title: USING THE NEW L BAND MSS ALLOCATIONS Study Group 8 Seminar on Tomorrows Technological Innovations Ge


1
USING THE NEW L BAND MSS ALLOCATIONS- Study
Group 8 Seminar on Tomorrows Technological
Innovations Geneva, 9 September 2004
  • Marcus Vilaça
  • Manager, Systems Engineering
  • Advanced Systems Division

2
Inmarsat Background
  • Established in 1979 as an international
    co-operative
  • Privatised in April 1999
  • Owns and operates 9 satellites 4 x Inmarsat 2
  • 5 x Inmarsat 3
  • Contract for 3 x Inmarsat 4 satellites signed in
    May 2000
  • Firmly established in maritime, aeronautical and
    land markets
  • Customer base of over 320,000 users
  • Current services include messaging, voice and
    data
  • Global presence network of suppliers of
    services and equipment
  • GMDSS

3
Inmarsat 1st Generation Space Segment
  • Marecs Marisat
  • 33 dBW EIRP 30 dBW EIRP
  • 2 x 5 MHz bandwidth 2 x 5 MHz
    bandwidth
  • 580 kg dry mass 360 kg dry mass
  • 13.5 m solar array 2.2 m (w) x 3.8
    m (h)
  • Launch A 20/12/81 (22/08/96)
    Launch 1 19/02/76
  • B 09/09/82 (F) 2 10/06/76
  • B2 10/11/84 (23/01/02) 3 14/10/76

4
Inmarsat 2
  • 39 dBW EIRP
  • 2 x 20 MHz Processed Bandwidth
  • 700kg Dry Mass
  • 14.5 m Solar Array Span
  • Launch F1 30/10/90
  • F2 08/03/91
  • F3 16/12/91
  • F4 15/04/92

5
Inmarsat 3
  • 49 dBW EIRP
  • 2 x 60 MHz Processed Bandwidth
  • 1000kg Dry Mass
  • 20.5 m Solar Array Span
  • Launch F1 03/04/96
  • F2 06/09/96
  • F3 18/12/96
  • F4 03/06/97
  • F5 04/02/98

6
Inmarsat 4
  • 67 dBW EIRP
  • 10 dB/K G/T
  • 2 x 126 MHz Processed Bandwidth
  • 9 m deployable reflector
  • 3000 kg Dry Mass
  • 6000 kg Launch Mass
  • 12 kW spacecraft power
  • 10 kW payload power
  • 48 m Solar Array Span
  • Astriums Eurostar 3000 bus
  • Major Subcontractors
  • TRW Astro
  • EMS
  • Alcatel
  • Boeing
  • Launch F1 February 2005
  • F2 July 2005

7
Inmarsat 4 Characteristics
  • Frequency Bands
  • Mobile Link _at_ L Band and Feeder Link _at_ C band
  • Transponders
  • Transparent bent-pipe, C/L, L/C, L/L, C/C
    Navigational
  • Digital Channeliser/Beamformer
  • 630 x 200 kHz channels, dynamically allocated to
    beams
  • 256 beams
  • Mobile Link (RHCP, digital beam former)
  • 228 narrow spot beams for BGAN service (1.1
    degree grid)
  • 19 wide spot beams for EE service (4.05 degree
    grid)
  • 1 global beam
  • Feeder Link (RHCP LHCP)
  • 1 global beam, dual polarisation

8
Inmarsat 4 Coverage

9
The MSS L Band Extension
10
Amethyst Programme
  • Part of the ESAs Artes 3 Line 4 study programme
  • Feasibility study focused on the changes required
    to the I4 payload design, to enable utilisation
    of the L band extension
  • Study lead by Astrium, supported by Inmarsat
  • Scenario 1 Modification of I4 flight model 3
    (FM3)
  • 1A - Minimum Changes
  • 1B - New DSP
  • Scenario 2 Procurement a fourth spacecraft
    (FM4)
  • 2A - New DSP
  • 2B - Enhanced SSPAs
  • Main Outputs Design Solutions, ROM Cost
    Development Plan

11
I4 Payload Block Diagram

12
I4 Frequency Plan
13
Baseline I4 L Band Pre-processor DSP

14
Scenario 1 - L Band Pre-processor DSP Changes

15
Scenario 1 Other Equipment Changes
  • L Band Feed
  • New diplexers
  • Feed element retuning
  • ONets
  • New output filters

16
Scenario 2 - L Band Pre-processor DSP Changes

17
Scenario 2 Other Equipment Changes
  • L Band Feed
  • New diplexers
  • Feed element retuning
  • ONets
  • New output filters
  • New SSPAs
  • Increased output power

18
Summary of Spectrum Issues

19
Planned Spectrum Activities
  • Studies into the use of the new bands and related
    sharing studies
  • Participation in the work being carried out by
    WP8D.
  • Regulatory study of the new bands
  • Assess the use of the new bands by existing
    terrestrial services, and the possibility of
    utilization of those bands for the provision of
    MSS in various countries, concentrating in Region
    1 and Region 3.
  • Satellite antenna discrimination
  • Analyse the impact of PFD limits on the service
    coverage area by taking into account satellite
    antenna discrimination performance.

20
Conclusion
  • The MSS L Band extensions offer a great
    opportunity to significantly increase the
    capacity of MSS satellites.
  • The modifications required to the baseline
    Inmarsat 4 satellites to allow service provision
    in the new bands are significant, but can be kept
    within limits that allow reduced risk and lower
    cost and schedule impact.
  • A comprehensive study on the utilisation of the
    extended L band by existing services will be
    carried out, to provide an accurate picture of
    the current situation and of any possible
    constraints.
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