MAXIM Data Systems Command & Data Handling Space - Ground Link Ground System 19 August 1999.
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Transcript of MAXIM Data Systems Command & Data Handling Space - Ground Link Ground System 19 August 1999.
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MAXIM Data Systems
Command & Data HandlingSpace - Ground Link
Ground System19 August 1999
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MAXIM Data Systems Topics
Data System Recommendations Options and Trades Spectrum Utilization Ground Antenna Capabilities Data System Drivers Data System Block Diagram Mass/Power Summary Operations Concept Link Margin Summary Cost Data Suggested Study Areas
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Recommendations for MAXIM
Detector satellite will transmit science data using S-Band to Optics Spacecraft for combined transmission to ground stations
Store data continuously & dump daily for 12 min using DSN 34M using X-Band
Total downlink data rate: 300 Kbps Use 2:1 data compression Use S-band for Optics/Detector transmissions Use S-band for backup comm from DSN for both Optics & Detector
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Options/Trades
Detector spacecraft to transmit telemetry to Optics spacecraft for combined relay to ground station ( vs separate links)
Less ground station time required Smaller antenna required for Detector Spacecraft & much simpler
communication system
Optics spacecraft sends recorded data vs real time Ground costs significantly less Allows good availability on DSN 34M system
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Options/Trades
DSN 34M recommended (vs 13M commercial) Allows hi-rate playback Reduces contact time Much lower cost Proven deep space operation 13 M commercial has unproven ranging capability at 40 million Km
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Spectrum Utilization
X-band Space to Ground Link (+) Uplink and downlink frequency assignments available (+) More efficient than S-Band (approx 11.5 dB) (+) S/C hardware is available (-) Rain attenuation (approx 2 dB)
S-band for Optics/Detector link (+ ) More efficient than X-Band (omni/omni) (+) Existing hardware available with modifications of frequency Rx/Tx (+) Allows backup to ground if needed (UHF not readily available)
S-Band to ground link (emergency) (0) Future allocation in DSN band may be questionable
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Ground Antenna Capabilities
DSN 34M: X-Band Rx/Tx
G/T = 52.4 dBi/K EIRP = 103 dBw max(can go to 110 dBw)
S-Band Rx/Tx G/T = 42.1 dBi/K EIRP = 98 dBw
13M commercial: X-Band Rx/Tx (uplink and ranging need to be added)
G/T = 37 dBi/K EIRP = 90 dBw
S-Band Rx/Tx G/T = 24.5 dBi/K EIRP = 68 dBw
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MAXIM Data System Drivers
Maximum Range: 40 million KM Daily Data Volume: 432 Mbits
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MAXIM Data Systems Block Diagram
X-bandXponder
&P wr A m p
Com m ands a 2 K bps
C& DH
S /C 1553B B US
OpticsS -bandXCV R
A CSS S R
BC
Sw
itch
Dip
lexer
S-bandXCV R
P layback @ 300 K bps
X-band Cm d/Tlm& Ranging
34M P rim e70M B ackup
DS NS tations
Com m ands
Telem etry
Sate llite d is h
S -band E m ergencyCm d/Tlm
MaximMOC
MaximScienceHSKP
X-band1.5 m HGA s
Hybrid
Dip
lexerX
X
S -band Om niA ntennas
Tlm @ 100 bpsCmd @ 12 bps H
ybrid
Dip
lexer
X
X
S -band Om niA ntennas
To/From Detector
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RF Communications Mass/ Power
X-band Transponder (2) 6 Kg Rx RxTx3 watt 32 wattsCont. for 1 hr/day
S-band XCVR &Diplexers (4)
14 Kg Rx RxTx10 watts 25 watts 1-2 hours/day
C&DH 4.5 Kg 30 watts
X-Band Antenna & ACU (2) 15 Kg 5 watts moving
S-Band OMNI (4) 2 Kg
Optics Spacecraft
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RF Communications Mass/ Power
S-band XCVR &Diplexers (2)
7 Kg 25 watts continuous
S-Band OMNI (2) 1 Kg
Detector Spacecraft
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DSN 34 M BWG(Stations at Canberra, Madrid, Goldstone)
MAXIMMOC
MAXIMScience Data
MAXIM Operations Concept Diagram
MAXIM Science
X-band Command @ 2 Kbps/Telemetry@ 300 Kbps and
Ranging
S-bandEmergency Command @ 12
bps/Telemetry @ 100 bps
S-band command and telemetry @ 4 Kbps
Telemetry (Housekeeping/Science)
Commands
S-band Emergency Command@ 12 bps and telemetry @ 100 bps
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MAXIM Operations Concept
Detector spacecraft will continuously transmit @ S-Band to Optics spacecraft @ 4 Kbps (3 Kbps science, 1 Kbps housekeeping, uncompressed)
Optics spacecraft will compress 2:1 all Detector data and 1 Kbps Optics housekeeping data
Optics spacecraft will continuously record all compressed data for playback 1/day for 12 min @ 300 Kbps to DSN 34M @ X-Band through 1 of 2 HGA antennas
Nominal commanding/ranging to Optics spacecraft will be done via
X-Band through DSN 34M BWG Both Optics & Detector will have S-Band low-rate command/telemetry
through DSN 34M for emergency operations Commands throughput from MOC, telemetry FTP’d from fileserver
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MAXIM Link Margin Summary
34 M BWG 13 M Commercial OMNI to Ground Spacecraft toSpacecraft
Downlink Rate 300 Kbps 7.5 Kbps 100 bits 4 Kbps
Uplink Rate 2 Kbps 2 Kbps 12 bits - - - - -
Contact Time 12 minutes 8 hours - - - - - - - - - -
Margin Downlink 3.5 dB 1.5 dB 0 dB 7.2 dB
Margin Uplink 2.5 dB 1.9 dB 0 dB - - - - -
Ranging Uplink 15.9 dB - - - - - - - - - - - - - - -
Ranging Downlink 21.0 dB - - - - - - - - - - - - - - -
All links have 3 dB required performance marginsAll links have rate 1/2 convolutional encoding
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Cost
Ground systems:
DSN 34M @ 1hr/day = $365k/yr x 3= $1.1M
13M commercial @ 8 hr/day = $7M
Optics Spacecraft: X Band
XPDRs(2) =$2M HGA antennas(2)= $2M
S-band XCVR(4) = $2.8M omni antennas(4) = $300K
C&DH = $2M
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Cost(cont’d)
Detector Spacecraft: S-band XCVR(2)= 1.4M omni antennas(2) = $150K
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Suggested Study Areas
Use of new coding schemes (e.g. Turbo Codes) Modified frequency scheme for S-band XCVR
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Acronym List
ACS - Attitude Control System ACU - Antenna Control Unit BC - Bus Controller BWG - Beam Wave Guide DSN - Deep Space Network FTP - File Transfer Protocol HGA - High Gain Antenna HSKP - housekeeping I/F - Interface MOC - Mission Operations Center RF - Radio Frequency SSR - Solid State Recorder XCVR - Transceiver XPDR - Transponder