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Roger Flaherty,

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MANAGEMENT OF THE TRACKING/DATA COMMUNICATIONS FACILITIES INCLUDING SPACE AND ... ICD/MOA/INOSP DEVELOPMENT ... ESTABLISHMENT OF LONG RANGE TECHNOLOGY ... – PowerPoint PPT presentation

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Title: Roger Flaherty,


1
Roger Flaherty, Deputy Program Manager GSFC Code
450 July, 2002
2
AGENDA
  • Mission Services Program Office Overview
  • Space Network
  • Ground Network

3
MISSION SERVICES PROGRAM OFFICE
THE MSPO IS RESPONSIBLE FOR PROGRAM PLANNING,
DIRECTION, AND OPERATION OF NASAs SPACEFLIGHT
TRACKING AND DATA NETWORK (STDN)
  • MANAGEMENT OF THE TRACKING/DATA COMMUNICATIONS
    FACILITIES INCLUDING SPACE AND GROUND NETWORKS
    AND SYSTEMS, PROVIDING DAY-TO-DAY SUPPORT OF
    LAUNCH AND ORBITAL ACTIVITIES
  • ICD/MOA/INOSP DEVELOPMENT
  • IMPROVEMENTS AND UPGRADES OF PRESENT NETWORKS
    SYSTEMS TO IMPROVE CURRENT USER SERVICE
    CAPABILITIES
  • ESTABLISHMENT OF LONG RANGE TECHNOLOGY
    INITIATIVES TO MEET FUTURE USER SERVICE
    REQUIREMENTS
  • PROVISION OF NETWORKS INSTITUTIONAL SUPPORT
  • CONTROL OF 530-SNUG (SPACE NETWORK USERS GUIDE)
  • CSOC CONTRACT MANAGEMENT

4
SPACE NETWORK
5
Space Network Concept
  • THE SPACE NETWORK (SN) WAS ESTABLISHED TO REPLACE
    NASAs WORLDWIDE NETWORK OF GROUND TRACKING
    STATIONS
  • THE SN DRAMATICALLY INCREASED TRACKING AND DATA
    ACQUISITION (TDA) COVERAGE FROM 15 TO 85 PER
    ORBIT OF LOW EARTH ORBITING SPACECRAFT AS WELL AS
    DECREASED OPERATIONAL COSTS
  • ADDITION OF THE GUAM REMOTE GROUND TERMINAL IN
    1998 FURTHER INCREASED TDA COVERAGE TO 100 FOR
    ALL CUSTOMERS BY PROVIDING CLOSURE TO THE TDRSS
    ZONE OF EXCLUSION
  • THE SN OPERATES AS A CUSTOMER DRIVEN BENT PIPE
    RELAY SYSTEM FOR TRACKING, TELEMETRY, AND COMMAND
    DATA

6
TDRSS COVERAGE
GODDARD SPACE
FLIGHT CENTER
WALLOPS FLIGHT
FACILITY
GUAM
254
94
174 TDW
TDW
321
41 TDE
121
355
195
127
47 TDS
275 TDZ
327
91
251
F-7
171 F-7
0/360
180W
-180W
TDRS VIEWS BASED ON 600KM USER ALTITUDE AT THE
EQUATOR
7
Tracking and Data Relay Satellites (TDRS)
First Generation TDRS F-1 through F-7
Second Generation TDRS F-8 through F-10
8
GROUND SEGMENT
  • WHITE SANDS COMPLEX (WSC)
  • TWO INDEPENDENT, FUNCTIONALLY IDENTICAL TDRS
    GROUND STATIONS LOCATED NEAR LAS CRUCES, NM FOR
    CONTROLLING THE TDRS
  • WSC ALTERNATIVE RESOURCE TERMINAL (WART) FOR
    TDRS-1 IN SUPPORT TO NSF
  • DATA SERVICES MANAGEMENT CENTER (DSMC)
  • OPERATIONAL HUB LOCATED AT THE WSC FOR
    COORDINATING ALL SPACE NETWORK ACTIVITIES
  • GUAM REMOTE GROUND TERMINAL
  • PROVIDES ZOE CLOSURE USING TDZ

9
White Sands Complex
  • TWO FUNCTIONALLY IDENTICAL, GEOGRAPHICALLY
    SEPARATED GROUND TERMINALS AT THE WHITE SANDS
    TEST FACILITY

THE WSC HAS FIVE SPACE TO GROUND LINK TERMINALS
(SGLTs) A SIXTH SGLT HAS BEEN INSTALLED AT THE
REMOTE GROUND TERMINAL ON GUAM AS AN EXTENDED WSC
SGLT THE WSC ALTERNATIVE RESOURCE TERMINAL
(WART) FUNCTION IS USED TO COMMAND AND CONTROL
TDRS-1 AND PROVIDES S-BAND (SSAF/SSAR) AND K-BAND
(KSAR) SERVICES TO NSF ONLY SERVICES UNABLE TO
SUPPORT ON-ORBIT USERS
10
DSMC FUNCTIONS
  • SERVICE PLANNING
  • DATABASE MANAGEMENT
  • ACRS (FORWARD AND RETURN LINK MUTUAL INTERFERENCE
    PREDICTION)
  • SCHEDULING
  • FORECAST PERIOD
  • ACTIVE PERIOD
  • CONFLICT RESOLUTION
  • MISSION OPERATIONS SUPPORT
  • EVENT MONITORING
  • REAL TIME FAULT ISOLATION

11
TDRSS SERVICES
  • MISSION PLANNING
  • REQUIREMENTS DEFINITION, ENGINEERING, AND
    INTEGRATION
  • COMMUNICATIONS LINK ANALYSIS AND SIMULATION
    SYSTEM (CLASS)
  • END-TO-END RF SYSTEMS ANALYSIS
  • TESTING
  • CHARACTERIZATION, AND VERIFICATION/VALIDATION
    TESTING FOR EVALUATING MISSION READINESS
  • INTERFACE COMPATIBILITY TESTING FOR RF AND GROUND
    DATA INTERFACES

12
TDRSS SERVICES (CONTD)
  • OPERATIONS PLANNING
  • DEVELOP AND COORDINATE THE IMPLEMENTATION OF
    APPROVED NETWORK ENHANCEMENTS TO SUPPORT NEW AND
    EVOLVING REQUIREMENTS
  • ENSURE SN ELEMENTS ARE PREPARED TO SUPPORT
    MISSION REQUIREMENTS. IMPLEMENT NECESSARY
    DATABASE CONNECTIVITIES.
  • PRE LAUNCH SUPPORT
  • PAYLOAD LAUNCH VEHICLE RF CHECKOUT
  • LAUNCH SUPPORT
  • TRACKING AND DATA ACQUISITION VIA TDRSS

13
TDRSS SERVICES (CONTD)
  • COMMAND
  • COMMANDS TRANSMITTED DIRECTLY VIA NISN TO WSC
  • WSC UPLINKS COMMANDS TO TDRS FOR RF TRANSMISSION
    TO CUSTOMER S/C
  • TELEMETRY
  • CUSTOMER DATA RECEIVED VIA TDRS AT WSC
  • WSC DOWN CONVERTS, DEMODULATES, BIT SYNCHRONIZES,
    CONVOLUTIONALLY DECODES, RECORDS DATA, AND SENDS
    ASYNCHRONOUS DATA TO NISN EQUIPMENT FOR
    TRANSMISSION TO CUSTOMERS IN IP OR ENCAPSULATED
    4800 BIT BLOCK FORMAT

14
TDRSS SERVICES (CONTD)
  • TRACKING
  • ONE-WAY DOPPLER FOR FREQUENCY DETERMINATION
  • RANGE USING DG-1 PN CODE AND 2-WAY DOPPLER
    TRACKING
  • CONTROL/STATUS
  • TDRSS LINK CONTROL MESSAGES AND PERFORMANCE
    MONITORING DATA

15
Service Summary/System Capacity
16
TDRSS/TDRS-H,I,J Baseline Service Comparison
SERVICE
TDRSS
TDRS - H,I,J
NOTES
300 kbps
FWD
300 kbps
S-BAND
RTN
6 Mbps
6 Mbps
SINGLE
NO CHANGE
FWD
ACCESS
25 Mbps
25 Mbps
Ku-BAND
RTN
300 Mbps
300 Mbps
FWD
N/A
25 Mbps
23/25-27 GHz frequency
Ka-BAND
band
RTN
N/A
800 Mbps
FOR TDRS H,I,J
SIMULTANEOUS
NUMBER OF
2 SSA
2 SSA
LINKS PER
OPERATION OF S Ku
2 KuSA
2 KuSA
AND S Ka SERVICES
SPACECRAFT
2 KaSA
A SINGLE SA ANTENNA
ARE REQUIRED
1 _at_ 10 kbps (8 dB
ANTICIPATED SSA
FWD
1 _at_ 10 kbps
NUMBER
over TDRSS)
USERS LESS THAN 3
MULTIPLE
OF
5 _at_ 150 kbps LIMITED BY GROUND EQ. ONLY
6 _at_ 3 Mbps (ONBOARD BEAMFORMING)
Mbps OFFLAOADED TO
ACCESS
LINKS
RTN
TDRS H,I,J MA
PER S/C
CUSTOMER TRACKING
150 meters 3 sigma
150 meters 3 sigma
NO CHANGE
Beyond 300 Mbps requires Ground Station
Modification
17
Demand Access Service (DAS)
  • DAS is an MA return service that utilizes 3 TDRS
    (F-3 F-7) nodes (0410W, 1740W, 2750W) to
    provide continuous global coverage.
  • A single user schedule can provide multi-year
    support
  • DAS automatically hands over from TDRS node to
    node for orbiting users
  • Data Rate from 1-150kbps/channel
  • Customers use TCP/IP interface
  • Low Cost based on node usage (subscription fee)
  • DAS Applications
  • Emergency/Contingency (911 service) customer
    transmits when problem occurs. DAS is always
    listening
  • Science Alerts Transmit when significant
    observations occur

18
Ka-Band Technology Development
  • In early 2000, NASA/GSFC initiated the Ka-band
    Transition Project as a first step in
    transitioning the SN and GN to Ka-band
    operations.
  • Project Goals
  • Develop new SN high rate telemetry service using
    TDRS H,I,J 650 MHz wide channel
  • Develop a GN station to demonstrate direct to
    earth Ka-band operations
  • Provide test bed within the SN and GN to
    demonstrate new communication technologies
  • High data rate demonstrations scheduled for fall
    2002
  • Ground Network
  • Implement a demonstration ground terminal for the
    Wallops Flight Facility to support direct to
    ground links in the 25.5 to 27.0 GHz band
  • Provide a 1200 MHz IF compatible with the SN
    implementation
  • Support unified S-band for command and
    housekeeping telemetry

19
Ka-Band Technology Development
  • Space Network
  • Upgrade SGLTs to take advantage of TDRS H,I,J 650
    MHz wide Ka-band channel
  • Add new Downconverters, Equalizers, and IF
    switching
  • Modify network control software for automated
    control and monitoring of new equipment
  • Provide Ka-band return signals at a 1200 MHz IF
    compatible with the GN IF interface
  • Accommodate SNIP space to space Ka-band frequency
    plan for both 225 MHz wide channel and the 650
    MHz wide channel
  • Space Network Ka-band Development Plan
  • Fiscal Year 2003
  • Complete system requirements
  • Complete Ops Concept
  • Complete System Spec
  • Fiscal Years 2004-2005
  • Hardware Development and testing
  • Demonstrations
  • Fiscal Year 2006
  • Establish Ka-band user services capability

20
ADVANTAGES OF SN SUPPORT SERVICES
  • SPACE-BORNE PLATFORM
  • READY ASSET
  • GLOBAL COVERAGE
  • QUICK DROP LOCK REACQ TIME
  • REDUNDANT PATHS (GROUND)
  • LOW MAINTENANCE OPERATIONS COST

21
Ground Network
22
(No Transcript)
23
Wallops Ground Station (WGS)
  • The primary antenna systems of the Wallops Ground
    Station (WGS) consist of three highly automated
    tracking systems. These systems provide support
    to low earth orbiting satellites. These include
    the 5-meter Low Earth Orbiter-Terminal (LEO-T),
    the 8-meter Transportable Orbital Tracking System
    (TOTS), and the 11.3-meter X- and S-Band tracking
    system.
  • The WGS provides an electronic interface between
    a spacecraft and a science user 24 hours per day,
    365 days per year. The 11.3-meter antenna system
    is shown in the foreground of the picture to the
    right.
  • Telemetry data is delivered in real-time or near
    real-time. For high data rate S-Band projects (gt
    10 Mbps) digital cassette tapes are available at
    a greatly reduced cost when compared to the
    dedicated circuit costs. Post pass playback of
    high rate recorded data can be scheduled. User
    generated commands are delivered to the
    spacecraft in throughput fashion and the 5-meter
    system can accept store-and-forward type
    commands.
  • Other tracking antenna systems used in support of
    low earth orbiting spacecraft at the WGS include
    7.3-meter L- and S-band antennas, various UHF
    arrays and an automated UHF yagi array providing
    support to the space station MIR.

24
AGS, Poker Flat Research Range, Chatanika, Alaska
  • The Alaska Ground Station (AGS) consists of two
    automated tracking systems. These systems are a
    5-meter Low Earth Orbiter-Terminal (LEO-T and an
    11.3-meter X- and S-Band tracking system. An
    8-meter Transportable Orbital Tracking System
    (TOTS) is prime for sounding rocket support but
    is available on a non-interference basis during
    high activity periods such as launch and early
    orbit operations. The station is located
    approximately 30 miles northeast of Fairbanks,
    Alaska. The station provides a beneficial
    tracking location for polar earth orbiting
    satellites due to its high latitude.

25
McMurdo Ground Station (MGS)
  • The McMurdo Ground Station (MGS) consists of an
    automated 10-meter tracking system. The station
    is located at McMurdo Station, Antarctica. The
    station provides a beneficial tracking location
    for polar orbiting satellites due to its high
    latitude. The primary functions of the station
    are the tracking and data acquisition of the
    Synthetic Aperture Radar (SAR) satellite systems,
    tracking and data acquisition of polar orbiting
    S-Band missions, and launch vehicle/payload
    tracking during launch and early orbit periods of
    high inclination missions. The station also
    includes the NASA Tracking and Data Relay System
    (TDRS) communications system.
  • Telemetry data can be delivered in real-time or
    near real-time using either the McMurdo TDRS
    Relay System (MTRS) or via a low-rate circuit.
    For high data rate S-Band projects (gt 10 Mbps)
    digital cassette tapes are available at a greatly
    reduced cost when compared to the communication
    circuit costs and can be air shipped to the user
    when shipping is available from the station. Post
    pass playback of high rate recorded data can be
    scheduled.

26
Svalbard Ground Station (SGS)
  • The Svalbard Ground Station (SGS) consists of an
    automated 11.3-meter tracking system. The station
    is located near the town of Longyearbyen on the
    Svalbard archipelago in Norway. Svalbard is
    located north-northeast of the main Norwegian
    land area. The station provides a beneficial
    tracking location for polar orbiting satellites
    due to its high latitude. The primary function of
    the station is tracking and data acquisition of
    the Earth Observing System (EOS) satellite
    missions.
  • Telemetry data can be delivered in real-time or
    near real-time using dedicated communications
    circuits back to NASAs Goddard Space Flight
    Center. For high data rate S-Band projects (gt 10
    Mbps) digital cassette tapes are available at a
    greatly reduced cost when compared to the
    dedicated circuit costs and can be air shipped to
    the user. Post pass playback of recorded data can
    be scheduled.

27
Mission Operations Support ContractConsolidated
Space Operations Contract (CSOC)
28
SCDS/CSOC Capabilities
  • Concept Definition (Phase A/B)Operations
    Concept Communications Architecture Mission
    Services Science Processing Concept Space
    Network/Ground Network(SN/GN) Utilization
    Analysis Flight Dynamics Concept Cost Benefit
    Analysis Cost Estimates Mission Life-Cycle
    Support Scenarios Risk Identification
    Mitigation Plan Information Security Plan
    Facility Requirements and Trade Studies
  • Design Development (Phase B/C/D)- Mission
    Documentation Design Flight Reviews Develop
    Deploy Mission, Communications SN/GN
    Systems/Assets SN/GN Loading Analysis Risk
    Management IntegrationTest(IT) Program
    Support and Facility Preparation- Pre-Launch
    Test Support Launch Site Support LaunchEarly
    Operations(LEO) Support (including ranging
    tracking, GPS Validation, Flight Dynamics, as
    appropriate)- Flight Operations Team(FOT)
    Training Certification Ops Procedures
    Development Verification Mission Database
    development and IT Operations
  • Flight Operations (Phase E) Flight Control
    Operations Mission/Science Planning Flight
    Dynamics Contingency Operations and Science
    Processing
  • Extended Flight Operations (Phase E)Transition
    to Extended Mission Mode (e.g. reduced support
    /or contacts, transfer to university)
  • Commercial Service ProvidersIdentify, acquire
    manage commercial service providers as required
    to augment NASA resources
  • Customer Support ServiceTrade Studies, SCDS/CSOC
    Support Coordination, Management of SN/GN
    Commercial provider GN Assets Services As
    Required

29
SCDS/CSOC Benefits
  • Depth of Resources provides right sizing during
    entire mission life Extensive experienced CSOC
    personnel base available for assignment at the
    right time. Multiple CSOC projects provide
    ability to efficiently manage personnel base.
  • Breadth of Resources tailored for your
    programCSOC personnel experience base includes
    the entire scope of mission requirements (e.g.
    R/F, SW, HW, FOT, IT, specialty engineering,
    subject matter experts). Personnel with relevant
    experience are assigned, thereby reducing
    technical risk to project and reducing cost
    through minimal learning curve activity.
  • Range of Resources provides optimal mission
    solutionNASA, non-NASA, commercial and custom
    capabilities will be selected and configured to
    provide the best solution.
  • Certified Redundancy Contingency Capabilities
    are available throughout mission lifeAlternate
    ground stations can be used to provide a robust
    backup capability (redundancy) in the event of HW
    failure, communications outage, etc. During
    critical mission activities (e.g. LEO,maneuvers,
    s/c anomalies), additional ground stations can be
    assigned to meet mission objectives
    (contingency).
  • On-Going Technology Refreshment Upgrade program
    alleviates obsolescenceIn partnership with GSFC,
    new technologies capabilities, upgrades and
    replacements are evaluated for application on a
    project by project basis. Cost/benefit analysis
    for NASA and Project is performed.
  • System Support Maintenance is pooled shared
    by multiple programs
  • Range of Mission Operations Concepts are
    available Included are dedicated shared FOTs
    at/near GSFC and dedicated remote FOTs (at
    customer facility).

30
RESOURCES
  • WDISC WEBSITE (SYSTEM INTERFACE AND REQUIREMENT
    DOCUMENTS ARE FOUND HERE)
  • http//msp.gsfc.nasa.gov/wdisc/
  • SPACE NETWORK ONLINE INFORMATION CENTER (DETAILED
    TRACKING AND DATA RELAY SATELLITE SYSTEM
    INFORMATION INCLUDING A LINK TO THE SN USER GUIDE
    REV. 7 (REV 8 COMING SOON))

31
BACKUP
32
Wallops Ground Station S-band Receive
33
Wallops Ground Station S-Band Transmit
34
Wallops Ground Station X-Band Receive
35
Alaska Ground Station S-band Receive
36
Alaska Ground Station S-Band Transmit
37
Alaska Ground Station X-Band Receive
38
McMurdo Ground Station S-band Receive
39
McMurdo Ground Station S-band Transmit
40
McMurdo X-Band Receive
41
Svalbard Ground Station S-band Receive
42
Svalbard Ground Station S-band Transmit
43
Svalbard X-Band Receive
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