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‘Production engineering a low cost video imaging
constellation’
10th IAA Symposium on Small Satellites for Earth Observation, Berlin, April 2015
Alex da Silva Curiel , Andrew Cawthorne, James Penson, Martin Sweeting
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1970 1975 1980 1985 1990 1995 2000 2005 2010
Nano
Micro
Mini
Small satellite trends
2
Cubesats and nanosats
PlanetLabs
Commercial ventures.
Commercialisation
RapidEye
UK-DMC Deimos-1
Beijing-1
EROS
Google SkyBox
exactEarth
DMC-3
WorldVu SpaceX GeoOptics SPIRE PlanetIQ GeoMetwatch Satellogic DAURIA etc….
Deimos-2
Comms and EO Constellations
Orbcomm Globalstar
AprizeSat
“Modern” Small satellite revolution
Military and techdemo
Small Satellite are the only way to deliver low latency global EO & comms services
2014
The opportunity......
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Num
ber o
f sat
ellit
es
SSTL – satellites produced per launch used
Introduction
• Since 2012 have been running an Internal R&D programme (designated ‘FIREWorks’) to develop the next generation of SSTL small satellite Platforms
• SSTL have introduced a new range of small satellites to the market – the X-Series
• The X-Series Satellites build on nearly 30 years of small satellite engineering experience
• The X-Series offer commercial level performance at extremely low recurrent cost, through a number of approaches: – Use of modern technologies, processes and protocols – Focusing on design for Automated production and Test processes and techniques
New Challenges and Opportunities
• Motivation and Stimulation – New Market Entrants, Extra competition, Need to Adapt & Evolve – New Technologies, protocols and techniques available from other
Sectors • Automotive Especially
– The Emergence of more Competitive Service based Models in the Markets – low data product prices required
– The evolution and Growth of SSTL • High Capital Investment in New Capabilities & Facilities • Experience in the successful use of COTs Technologies on Small Satellites
5
2000s 1980’s 1990’s 2012
Introducing the SSTL X-Series • A new range of platforms with common core features
• A single system architecture and technology designed to meet
all mission applications and requirements across the entire range.
• Common, modular and expandable specification • available on all platforms and missions:
– Dual redundant systems – Data storage up to Terabytes capacity – Data bus transfer rates of Gigabits per second – Onboard real-time processing of
Giga-instructions per second – High speed X-Band downlink
SSTL NovaSAR
SSTL 300 S1
SSTL 300
SSTL GMP-T
SSTL 150
SSTL 100
SSTL-X50
Cubesats
Majority of LEO SSTL Platforms will be X-Series in next 3-5 years
Design Principles
• Retain Core SSTL Design Principles, built up over 30 years – Simplicity – Robustness – Hands off Operations – Simple Safe Modes – Use of COTs Technologies
• Make Use of New Techniques
& Technologies – Automated Manufacture – Automated Test
• Employ Card Frame Based Core
Avionics Architecture – Provide Modularity & Flexibility
1980
1990
2010
2000
Modularity & Flexibility SSTL-X300 – S1 Block Diagram
9
IOB_0(Connections TBD)
LIN
CA
N
CA
N-F
D
AD
Cs
RS4
22
RS4
85
PWM
s
TT&C
AOCS
XTX_0XTX_1
MTQ X
MTQ Y
MTQ Z
PWM
PWM
PWM
WHL_0
RS485
CAN
BC
M_0
LIN
SAin_0
SAin_1
BC
M_1
LIN
SAin_0
SAin_1
S-TR
x_0 LIN
CAN
CAN
CAN-FDRx_Ant
Tx_LR
Tx_HR
S-TR
x_0 LIN
CAN
CAN
CAN-FDRx_Ant
Tx_LR
Tx_HR
PIU
_0(C
onne
ctio
ns T
BD
)LIN
CAN
CAN-FDHSL
LVDS
OB
C_0
LIN
CAN
CAN-FD HSL
SpWr
OB
C_1
LIN
CAN
CAN-FD HSL
SpWr
IOB_1(Connections TBD)
LIN
CA
N
CA
N-F
D
AD
Cs
RS4
22
RS4
85
PWM
s
STRK
_0
STRK
_1
MTM_0 RS422
MTM_1 RS422
GYRO_0 RS422
GYRO_1 RS422
SUNSEN_0ANLG
SUNSEN_1ANLG
SUNSEN_2 ANLG
SUNSEN_3 ANLG
WHL_1
RS485
CAN
WHL_2
RS485
CAN
PDM_0
Switc
hes
LIN
PAYLOAD CHAIN
PROPULSIONHEATER_0Switch
HEATER_1Switch
HEATER_2Switch
HEATER_3Switch
PIU
_0(C
onne
ctio
ns T
BD
)LIN
CAN
CAN-FDHSL
LVDS
APM_0APM_1
WHL_3
RS485
CAN
SGR Axio 0CANSwitch
IOB_2(Connections TBD)
LIN
CA
N
CA
N-FD
AD
Cs
RS422
RS485
PWM
s
BC
M_2
LIN
SAin_0
SAin_1
+X
IOB_3(Connections TBD)
LIN
CA
N
CA
N-FD
AD
Cs
RS422
RS485
PWM
s
SGR Axio 1CANSwitch
---------
LIN
CAN
CAN-FD
HSL
A point-to-point link
Power node (with distributed switch)
CAN ordinaire node
Higher Speed CAN
Payload Chain High Speed Link
BC
M_3
LIN
SAin_0
SAin_1
BC
M_4
LIN
SAin_0
SAin_1
-Z
BC
M_5
LIN
SAin_0
SAin_1
-Z
WHL_4
RS485
CAN
WHL_5
RS485
CAN
WHL_6
RS485
CAN
WHL_7
RS485
CAN
TANK_0
TANK_1
UHRI
TANK_2
MM
ULIN
CAN
HSL
MM
ULIN
CAN
HSL
TT&C
POWER
AOCS
XTX_0 XTX_1
SLIM6
MTQ X
MTQ Y
MTQ Z
PWM
PWM
PWM
WHL_0
RS485
CAN
BC
M_X
LIN
SAin_0
SAin_1
BC
M_Y
LIN
SAin_0
SAin_1
S-TR
x_0 LIN
CAN
CAN
CAN-FDRx_Ant
Tx_LR
Tx_HR
S-TR
x_0 LIN
CAN
CAN
CAN-FDRx_Ant
Tx_LR
Tx_HR
PIU
_0(C
onne
ctio
ns T
BD
)LIN
CAN
CAN-FDHSL
LVDS
OB
C_0
LIN
CAN
CAN-FD HSL
SpWr
OB
C_1
LIN
CAN
CAN-FD HSL
SpWr
IOB
_0(C
onne
ctio
ns T
BD
)
LIN
CAN
CAN-FD
ADCs
RS422
RS485
PWMs
IOB
_1(C
onne
ctio
ns T
BD
)
LIN
CAN
CAN-FD
ADCs
RS422
RS485
PWMs
MTM_0 RS422
MTM_1 RS422
GYRO_0 RS422
GYRO_1 RS422
SUNSEN_0ANLG
SUNSEN_1ANLG
SUNSEN_2 ANLG
SUNSEN_3 ANLG
WHL_1
RS485
CAN
WHL_2
RS485
CAN
PDM
_0
Switches LIN
PAYLOAD CHAIN
IOB
_2(C
onnections TBD
)
LIN
CAN
CAN-FD
ADCs
RS422
RS485
PWMs
PROPULSION
PROPTANK
0
HEATER_0Switch
HEATER_1Switch
HEATER_2Switch
HEATER_3Switch
PLENUM_0
PIU
_0(C
onne
ctio
ns T
BD
)LIN
CAN
CAN-FDHSL
LVDS
STRK
_0
STRK
_1
---------
LIN
CAN
CAN-FD
HSL
A point-to-point link
Power node (with distributed switch)
CAN ordinaire node
Higher Speed CAN
Payload Chain High Speed Link
SGR Axio 0CANSwitch
SGR Axio 1CANSwitch
SSTL – X-50 Block Diagram
• Common Building Blocks • Configurable to suit different
capacity & capability requirements
What could you fly? • Low cost constellation platform • Configurable structure and solar arrays • User focuses on the mission and payload
10
Space avionics production line
• To take advantage of the evolution of component technology • Reduces possibility of damage to SMT devices from hand soldering • Reduce the schedule and cost of manufacturing • Reduces manufacturing cost of PCA’s • Build into stock
• Process design and space qualification has required extensive effort
* Equipment type for illustrative purposes
Stencil Printer Reflow Machine X - Ray Machine (Pick and Place)
Automated Optical Inspection Cleaning
Production Cost Efficiency
• Step Change in Production Costs achieved through use of: – Component Pick & Place – Automated Solder (Re-flow) – Automated Inspection – Automated Test
• Automated Testing of system at Platform Level
12
Approach Scenario
Traditional/ Bespoke
COTs Manual
COTS Automated
Prod
uctio
n Ph
ase
Dura
tions
Procurement Weeks Days Days
Assembly Weeks Weeks Hours
Inspection Days Days Hours
Test Weeks Weeks Hours Overall Months Weeks/
Months Days
First Products to Market - The X-50 Series
• Essentially Re-Packages the current SSTL-100 in to a smaller, lower cost package
• Add improved capabilities
SSTL-100 platform SSTL-X50 platform
Series of x50 Platforms • Many Applications and three reference products:
– Medium Resolution EO (‘Earthmapper’) – 2.5m EO (‘Precision’) – Medium Resolution Multispectral & SWIR (‘True Colour’)
14
SWIR NIR R G B
NIR R G
pan
X50 microsat systems Earthmapper
22m GSD 600km swath
“Earth landmass,
daily” TrueColour 5m GSD
390km swath
Precision 0.7m GSD
1m HD video
R G B
Training and Development • Hands-on • On-the-Job Mission Control Centre
Launch and Insurance
EarthMapper • Never miss an image – always on over sunlit land
• 660km swath, 22m resolution
• One satellite covers the earth in 5 days, five satellites in one
day, guaranteeing an image before and after every event on
the ground
• For agricultural and disaster monitoring, water, national, global
and urban mapping
• Imagery typically only found on Large Institutional Missions
• High 5m Resolution Imagery, with 19m SWIR
• Wide 390km Swath for large area coverage
• For Mapping, Vegetation, Land Cover, Floods and Water,
Disaster Management, Urban and Geological Mapping
TrueColour+
Precision • Very High 0.7m Resolution Imagery
• 1m HD Full Motion Video
• Existing Markets – Mapping, Agriculture, Security, Insurance
• Emerging Markets – Financial and Economic Modelling,
Consumer Media, Competitor Analysis
Precision – Colour HD Video Specification
Spectral Bands HD Video: PAN or colour, Still: Red, Green, Blue, NIR
GSD HD video: 1 m, Still imagery: 0.7 m, Both modes from the same payload
Swath Video mode in 2.5xk2k HD format, Still image mode 17 km swath
Field of Regard +/- 40o , Equivalent to 750 km on the ground
SNR All bands > 100:1 Data Products Radiometrically and geometrically calibrated, 12 bits/pixel Compression Ratio Lossless up to 2.5:1, Lossy at higher ratios
Mass 60 kg to 160 kg dependent on configuration Redundancy Dual redundant systems Reference Orbit 500km, SSO, 10.30am LTAN Data Storage Up to 1 Tbyte Downlink 80-500 Mbits per second Design life 5 years+ Revisit 2 times daily above lower latitudes for 5 satellite constellation
Data capacity 640 – 960 image scenes per day (17x17km) 185,000 to 280,000km^2 per day
Conclusions • The next generation of SSTL small satellite platforms has
been described, the X-Series, designed for automated manufacture and test.
• The SSTL-X50 “Precision“ mission addresses the need for commercial operational constellations providing high resolution imaging and video.