Deep Space Network. November 17, Michael Rodrigues Manager Deep Space Network Program Jet Propulsion Laboratory
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1 Deep Space Network November 17, 2009 Michael Rodrigues Manager Deep Space Network Program Jet Propulsion Laboratory
2 NASA Networks Viewing Capabilities MJR 2 (11/17/09)
3 DSN can provide continual tracking to spacecraft above 30,000 km (including the Moon) Space Network (SN) can provide continual tracking to spacecraft below GEO Near-Earth Network (NEN) can provide short passes with high performance to LEOs NASA Networks: DSN, SN, and NEN Madrid View Goldstone View Earth Canberra View Moon is thataway at 10x GEO GEO 30,000 Km LEO (600 Km) Creates opportunities for NASA network redundancy and interoperability View looking down on the Earth s North Pole MJR 3 (11/17/09)
4 Deep Space Network - Today MJR 4 (11/17/09)
5 DSN Facilities DSS-24 34m (BWG-1) DSS-25 34m (BWG-2) DSS-26 34m (BWG-3) DSS-27 34m (HSB) DSS-54 34m (BWG-1) DSS-55 34m (BWG-2) DSS-34 34m (BWG-1) DSS-35 34m (in 2015) DSS-28 34m (HSB) DSS-63 DSS-43 DSS-14 Signal Processing Center SPC-10 Signal Processing Center SPC-60 Signal Processing Center SPC-40 DSS-15 34m HEF Goldstone, California GPS DSS-13 34m (**R&D) DSS-65 34m (HEF) Madrid, Spain GPS DSS-45 34m (HEF) GPS Canberra, Australia CTT-22 Compatibility Test Trailer MIL-71 Launch Support Facility at KSC JPL, Pasadena Network Operations Control Center (NOCC) ITT, Monrovia Service Preparation, Logistics, Compatibility Testing, O&M Analysis MJR 5 (11/17/09)
6 DSN Configuration: Today S-Band Radar Goldstone Supports over three dozen missions 34m HEF Madrid Interoperable w/other CCSDS conforming assets Spectral Bands: S (Cat. A & B) X (Cat. A & B), Ka 26, Ka 32/34 34m HEF 34m HEF Canberra Services: Downlink (telemetry) Uplink (command) Radiometrics (Doppler, Ranging, Delta-DOR) Radio Science VLBI CCSDS protocols (CFDP & SLE) Emergency Services MJR 6 (11/17/09)
7 WAN Bandwidth - Today MDSCC T3 ( 45 Mbps ) T3 ( 45 Mbps ) Madrid POP 26 Mbps Primary 2 Mbps (videoconferencing ) GSFC (B14) 26 Mbps Backup (MDSCC GDSCC ) 5 Mbps Backup ( GDSCC MDSCC) GSFC (B32) Lockheed Martin White Sands 1.5 Mbps ( ECC-LMSCC)*** 5 Mbps Backup ( GDSCC JPL) 32 Mbps Backup (GDSCC JPL) AT&T (Glendale ) T3 ( 45 Mbps ) GDSCC Verizon / Ft. Irwin T 3 (45 Mbps) 37 Mbps Primary AT&T (La Crescenta )** JPL Symmetrical bandwidth service Asymmetrical bandwidth service T3 Circuit 26 Mbps Backup NISN NTR Backbone CDSCC T3 (45 Mbps) T3 (45 Mbps) Sydney POP 26 Mbps Primary 2 Mbps (videoconferencing) GDSCC?? JPL (primary) GDSCC? JPL (via White Sands) JPL? GDSCC (via White Sands) 37 Mbps 32 Mbps 5 Mbps CDSCC? JPL 26 Mbps CDSCC? GDSCC 26 Mbps MDSCC? JPL FY09/10 26 Mbps MDSCC? GDSCC 26 Mbps GDSCC? MDSCC 5 Mbps ** CDSCC primary circuit move to La Crescenta POP in progress ( currently routed via Glendale) *** in progress MJR 7 (11/17/09)
8 34-m Beam Waveguide Antennas f 1 Shaped-Surface Subreflector 34m Shaped Surface Reflector Geometric Foci Beam Waveguide f 2 Azimuth Track Pedestal Room f 3 Microwave Packages MJR 8 (11/17/09)
9 Trend of Service Requested/ delivered MJR 9 (11/17/09)
10 Demand on 70-m Link Capacity (Aug 09) 16% of passes tracked on 70-m s requires 70-m capacity Used by Cassini, Spitzer and surprisingly SOHO 15% of passes tracked on 70-m s could be supported by an array of two 34-m 67% of passes tracked on 70-m s could be supported by a single 34-m MJR 10 (11/17/09)
11 Metrics DSN Network Data Delivery 12-Month Rolling Average MJR 11 (11/17/09)
12 Deep Space Network Future Plans MJR 12 (11/17/09)
13 DSN Configuration: ~2018 Goldstone 34m HEF Madrid Ensure robustness of DSN services: Replace, repair and modernize; comply with ES&H requirements Add capacity to balance North/South (at Ka) Provide backup to antennas across the network 34m HEF Canberra New Antennas One at each site equipped with 80 kw X- band uplink 34m HEF All s equipped with Ka-band MJR 13 (11/17/09)
14 DSN Configuration: 2023 Goldstone 34m HEF Madrid 34m HEF Canberra One new 34m antenna at each complex provides redundant capability Additional antennas can be added as need antennas may continue to be operable Provision of Radar capability TBD 34m HEF MJR 14 (11/17/09)
15 DSN Configuration Increased Capabilities: Mars Downlink Data Rate Possibilities Spectral Band Spacecraft Transmitter Power Notes Data rate, Closest (0.6 AU) Data rate, Farthest (2.6 AU) m antenna X-Band 100 Watts MRO-class today * 20 Mbps 1 Mbps m antenna Ka-Band 35 Watts Feasible today 28 Mbps 1.5 Mbps m antennas or equivalent m antenna or equivalent m antennas or equivalent Ka-Band 35 Watts DSN Goal 84 Mbps 4 Mbps Ka-Band 180 Watts Transmitter already developed and commercialized (LRO, Kepler) 144 Mbps ** 8 Mbps Ka-Band 180 Watts DSN Goal 432 Mbps ** 23 Mbps * Reference spacecraft is MRO-class (power and antenna), Rate 1/6 Turbo Coding, 3 db margin, 90% weather, and 20 DSN antenna elevation. Actual MRO mission achieves less at closest approach due to bottlenecks in data handling ** Performance will likely be 2 to three times lower due to need for bandwidth-efficient modulation to remain in allocated spectrum MJR 15 (11/17/09)
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