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BP/LD/BG - 15/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology
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A Vision for theNext GenerationDeep Space NetworkBob PrestonChief ScientistInterplanetary Network Directorate, JPL
Les DeutschArchitecture and Strategic PlanningInterplanetary Network Directorate, JPL
Barry GeldzahlerProgram Executive, Deep Space NetworkScience Mission Directorate, NASA
BP/LD/BG - 25/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology
The Challenge for Deep Space Communications
• Over the next 30 years deep space communication will have to accommodate orders-of-magnitude increase in data to and from spacecraft and at least a doubling of the number of supported spacecraft
• The present DSN architecture is not extensible to meet future needs in a reliable and cost effective manner
• NASA must develop a new strategy for deep space communications that meets the forthcoming dramatic increase in mission needs
BP/LD/BG - 35/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology
What is the Present Deep Space Network?
CanberraGoldstone
Madrid
• Three major tracking sites around the globe, with 16 large antennas, provide continuous communication and navigation support for the world’s deep space missions
• Currently services ~ 35 spacecraft both for NASA and foreign agencies– Includes missions devoted to planetary, heliophysics, and astrophysical
sciences as well as to technology demonstration• Spigot for science data from most spacecraft instruments exploring the
solar system, as well as a critical element of radio science instruments• A $2B infrastructure that has been critical to the support of 10’s of $B of
NASA spacecraft engaged in scientific exploration over the last few decades
BP/LD/BG - 45/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology
Why Does NASA Need a Next Generation DSN? • Many of the current DSN assets are obsolete or well beyond the end of their
design lifetimes– The largest antennas (70m diameter) are more than 40 years old and are not suitable for
use at Ka-band where wider bandwidths allow for the higher data rates required for future missions
– Current DSN is not sufficiently resilient or redundant to handle future mission demands
• Future US deep space missions will require much more performance than the current system can provide
– Require ~ factor of 10 or more bits returned from spacecraft each decade– Require ~ factor of 10 or more bits sent to spacecraft each decade– Require more precise spacecraft navigation for entry/descent/landing and outer planet
encounters– Require improvements needed to support human missions
• NASA has neglected investment in the DSN, and other communications infrastructure for more than a decade
– Compared to 15 years ago, the number of DSN-tracked spacecraft has grown by 450%, but the number of antennas has grown only by 30%
• There is a need to reduce operations and maintenance costs beyond the levels of the current system
BP/LD/BG - 55/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology
NASA’s Science Missions are Changing
Low-Earth-orbit solar and astrophysical observatories.
Single, large spacecraft for solar & astrophysics obs.
Preliminary solar system reconn. via brief flybys.
In situ exploration via short-lived probes.
Observatories located farther from Earth.
(e.g., Spitzer, JWST)
Constellations of small, low-cost spacecraft.(e.g., MMS, MagCon)
Detailed Orbital Remote Sensing.
In situ exp. via long-lived mobile human &
robotic elements.
• MGS, Mars Odyssey, & MRO will obtain high resolution images of only about 1% of Mars surface
– Data rate is a constraint on the ability to understand the planet• Science and human exploration missions need remote sensing as now done for the Earth
509/09/05Evolution of the Deep Space NetworkEvolution of the Deep Space Network
BP/LD/BG - 65/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology Doing Similar Remote Sensing at
Other Planets as We do Today at Earth
Required Improvement
Synthetic Aperture Radar
DATARATES(bits/s)
Data for ScienceData for Science
Data for PublicData for Public
1E+04 1E+05 1E+06 1E+07 1E+08
Planetary Images
Video
Multi-Spectral & Hyper-Spectral Imagers
HDTV
Direction of IncreasingData Richness
Direction of IncreasingSense of Presence IMAX
Cassini CommunicationCapability
BP/LD/BG - 75/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology
The DSN and Outer Planets Missions
Relative DifficultyPlace Distance Difficulty
Geo 4x104 km Baseline
Moon 4x105 km 100
Mars 3x108 km 5.6x107
Jupiter 8x108 km 4.0x108
Pluto 5x109 km 1.6x1010
A capable DSN is especially critical to outer planetmissions since communication is much more difficultcompared to the inner solar system
BP/LD/BG - 85/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology
1
10
100
1,000
10,000
100,000
1,000,000
2005 2010 2015 2020 2025 2030
Dow
nlin
k R
ate
(Kbp
s) Projected Downlink Rate500 MHz of Ka Bandwidth
Max RateAve Rate
DSN’s Future Mission Drivers
1.E+00
1.E+01
1.E+02
1.E+03
1.E+04
1.E+05
1.E+06
1.E+07
2005 2010 2015 2020 2025 2030
Projected Downlink Difficulty
(kbp
s x
AU
2 ) Max Link Difficulty
Ave Link Difficulty
0
20
40
60
80
100
120
2005 2010 2015 2020 2025 2030
Projected Number of Downlinks
Links
Spacecraft
Missions
• Probable future DSN mission sets are frequently analyzed – All NASA missions beyond
geosynchronous Earth orbit– Science and exploration missions
• Analysis shows that by 2030 DSN must be ready to support:– 1000X downlink performance increase
(likely more for certain missions)– 2X number of spacecraft increase
BP/LD/BG - 95/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology
DSN Performance Gap
1 bps
1 Kbps
1 Mbps
1 Gbps
1 Tbps
1 Pbps
10,000 km 100,000 km 1 Mkm 10 Mkm 100 Mkm 1 Bkm 10 Bkm 100 Bkm
GEO Moon MarsJupiter
PlutoEdge of Solar System
Current DSN Sensitivity
(70m antenna at X-band)
Mission Requirements out to 2030
• 1,000-fold increase is needed to support planetary missions• Adequate sensitivity already exists for all lunar and Earth libration point missions
BP/LD/BG - 105/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology
Planning for the DSN Future
• NASA and JPL have generated a roadmap for the DSN based on requirements derived from analysis of probable future mission sets
• This DSN roadmap is being integrated into an overall NASA Space Communications Program Plan by the NASA Space Communications Architecture Working Group (SCAWG)
• The SCAWG made recommendations about the future of space communications to the NASA Administrator (Griffin) and the NASA Strategic Management Council
• The NASA Administrator declared that NASA has neglected the DSN and communications infrastructure investment and asked that a plan be ready to deliver to Congress in February 2007
Planning process:
BP/LD/BG - 115/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology
A Plan for the DSN Future
• Radio communication with large arrays of small antennas will be the backbone of deep space communications (#2 recommendation of SCAWG, after next generation TDRSS)
– Would serve all missions, large and small, new and old
– Technology is mature and low-risk
– Costs will be recovered over time through reduction of DSN operations and maintenance costs
• Orbital data relays at the Moon, Mars, and perhaps other planets will allow the highest possible communication volumes from spacecraft at those bodies
• Optical communication would allow the transfer of extremely high data rates on “trunk lines” from Mars or the Moon to Earth, or for special missions (but would require implementation of an extensive reception infrastructure)
Recommended key elements of future DSN:
BP/LD/BG - 125/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology
The Next Generation DSN: Arrays of Small Antennas
Arrays of small radio antennas will provide:
• More resilience and redundancy: – Graceful degradation in performance in case of antenna
or receiver failures – fewer single points of failure
• Much greater data flow to and from spacecraft:– Meets the data rate requirements of most future NASA
missions and instruments
• Easily scalable architecture when growth is required
• Significant growth in the number of spacecraft that can be simultaneously tracked
– Each with just the required aperture
• Higher precision spacecraft navigation– Required for precision entry/descent/landing and for
outer planet exploration• Improved cost-effectiveness
– Substantially reduces operations and maintenance costs: Plug-and-play components with longer lifetimes
BP/LD/BG - 135/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology
Arrays: What Has Already Been Accomplished
U.S.Australia
DSN arrays enabled Galileo to succeed after its HGA failed to deploy
6-m DSN Array breadboard antenna
1309/09/05
• Radio astronomers have used arrays since the 1970s
• DSN supported Voyager’s Uranus and Neptune encounters with arrays of antennas (including international radio telescopes)
• DSN helped save Galileo through routine use of antenna arrays (including Parkes)
• Mid 80s plan to expand DSN with 34m antennas rather than 70m assumed arrays
– DSN currently offers 34m arraying as a standard service (used often by Cassini)
• Array breadboard task is underway as a technology demonstration
– Developing 3 antennas (6- and 12-m diameter) and components that can be mass-produced for low cost
– Demonstrating signal combining algorithms
BP/LD/BG - 145/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology
End-to-End RF Communication Performance
Current DSNSpacecraft: X-band, 10W, 1.5m ant; DSN: 70m ant
Next Gen DSN AntennasFactor of 10 over today’s 70m
Advanced Coding & CompressionFactor of 5 over today
Ka-Band Deployment on all AssetsFactor of 4 enabled by Next Gen DSN
High Power S/C Transmitter100W
1
10
100
1000 Flight Enhancements
Ground Enhancements
Flight/Ground Enhancements
Per
form
ance
Impr
ovem
ent
• Future end-to-end communication performance will rely on more than just improvements to ground facilities
• Additional enhancements are under development
• X 1,000 performance increase possible for most deep space missions• Some missions might achieve more – up to 1,000,000
– Via higher power transmitters, larger spacecraft antennas, or optical communication
BP/LD/BG - 155/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology
Example Benefits of Future DSN to NASA Missions
• Orders of magnitude increase in downlink data rates– Video instead of single images– Improved multi-spectral imaging
• Increased temporal and/or spatial resolution• Increased wavelength and/or geographical coverage
– Room to grow to support the human exploration era• Including intense robotic exploration of Mars
• Orders of magnitude increase in up uplink data rates– Enables expected growth of software uploads and human
communication needs• Same instrument performance much farther from Earth• Direct-to-Earth transmission can enable new mission
concepts for probes, rovers, and balloons– Hemispherical planet coverage (e.g., for multiple probes,
longer communication periods)– Improved position/velocity measurements (e.g., for winds)
• Improved mission parameters/cost– Higher link sensitivity could be used to lower spacecraft
power, mass, pointing accuracy requirements, …• Improved data-rate from low-gain antennas during descent
and landing or spacecraft emergencies
Single high performance user, or
Multiple users on sub-arrays
Flexibility of the Array Architecture
BP/LD/BG - 165/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology DSN: Looking Forward
1.E-06
1.E-04
1.E-02
1.E+00
1.E+02
1.E+04
1.E+06
1.E+08
1.E+10
1.E+12
1950 1960 1970 1980 1990 2000 2010 2020 2030
Base
line
(Firs
t Dee
p Sp
ace
mis
sion
)
3-W
, 1.2
-m S
-Ban
d A
nten
na (S
/C)
Red
uced
Tra
nspo
nder
Noi
se (S
/C)
Mas
er (G
) 10-W
S-B
and
TWT
(S/C
)64
-m A
nten
na (G
)R
educ
ed M
icro
wav
e N
oise
(G)
Red
uced
Ant
Sur
f Tol
eran
ces
(G)
Impr
oved
Ant
enna
(G)
Inte
rple
xed,
Impr
oved
Cod
ing
(G &
S/C
)X-
Ban
d M
aser
(G)
Con
cate
nate
d C
odin
g (7
, 1/2
) + R
-S (G
& S
/C)
3.7-
m X
-/X-B
and
Ant
enna
(S/C
)A
rray
: 64-
m +
1 3
4-m
(G)
Red
uced
Mic
row
ave
Noi
se (G
)
Vid
eo D
ata
Com
pres
sion
(G &
S/C
)70
-m A
nten
na (G
)A
rray
: 70-
m +
2 3
4-m
(G)
Impr
oved
Cod
ing
(15/
1/6)
(G &
S/C
)
Equ
ival
ent D
ata
Rat
e fro
m J
upite
r
Pioneer IV
Mariner IV
Mariner 69
Mariner 10
Voyager
Galileo
100W
Ka-
Ban
d Tr
ansm
itter
(S/C
)
DS
N A
rray
-Pha
se 2
(G)
1kW
Ka-
Ban
d Tr
ansm
itter
(S/C
)
Adv
ance
d C
odin
g an
d C
ompr
essi
on (G
& S
/C)
10.5
m S
pace
craf
t Ant
enna
(S/C
)
DS
N A
rray
-Pha
se 1
(G)
Ka-
Ban
d S
yste
ms
(G &
S/C
)
1.5-
m S
-/X-B
and
Ant
ena
(S/C
)
MRO
Kepler
20-W
S-B
and
TWT,
Blo
ck C
odin
g (G
& S
/C)
LJD - 1611/18/04
Opt
ical
Com
m
BP/LD/BG - 175/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology
Today’s DSN
Global coverage of Deep SpaceCurrent state of the art
Optical Communications
High bandwidth communicationsLow mass spacecraft componentsBeginning of technology growth curve
NASA Space Networking
High reliabilityHigh Performance: ≥ x1000 by 2015Cost effectivePlanetary networks, seamless connectivity
DSN Array
Modular and expandableLow cost manufacturing and operationsx40 performance
Planetary Networks
High performance explorationIncreased accessibilityImproved navand position locations
1706/25//05Evolution of the Deep Space Network
BP/LD/BG - 185/4//06
Next Generation DSNNational Aeronautics and Space AdministrationJet Propulsion LaboratoryCalifornia Institute of Technology
Summary
• NASA mission models indicate that orders-of-magnitude growth in network capacity are required over the coming decades
• To meet these future requirements a new end-to-end DSN architecture is envisioned that includes antenna arrays, local networks at the Moon and Mars, and eventually optical communications on some links
• All subsequent NASA deep space missions would be orders-of-magnitude more science-capable
• The schedule for implementation of the next generation DSN will depend on NASA budgetary and programmatic decisions, in addition to the pressure of future mission requirements
– The science community is free to express their opinion to NASA
• Until the new DSN is in place NASA is committed to ensuring that the current DSN can meet mission commitments