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Innovations in Small Satellites
and On-Orbit Manufacturing
TripleSat Constellation
Credit: SSTL
Video from Low Earth Orbit
• Historically, providing video from space has been
tricky:-
– Having enough satellite or sensor agility to keep
a single location in view for the duration of a
short pass (5-10 mins) has been challenging
– Spatial resolution has been low
– The data rates generated by the camera have
posed issues for on-board storage, data
downlink, or both
– Availability of ground stations for real-time
control has been a problem
• But video from space is coming, enabled by
improved bus technologies
The Carbonite Programme
Carbonite ‘s current capability
• Low-cost, high-resolution rapid response
experimental EO mission
• Mass = 80kg
• Colour high definition video
• Direct delivery to users
• Designed and built in 7 months
• Carbonite-2 under construction
(1-metre resolution – post-processed to 0.5-metre)
Carbonite ‘s future iterations
• 0.5m to 1m resolution
• Full colour, stills and HD video
• 1400 images per day
• 450s video per day
• <50kg
• 3 months to launch
Low-Elevation Mode Imaging
Multiple Imagery Collection Modes
Highly Agile Single Scene Imaging Extended Strip Imaging
In-pass Stereo Mode Imaging
Area Mode Imaging
12
Super-Resolution Mode Imaging
Strip 1
Strip 2
Strip 3
Strip 4
Manoeuvre
time
Manoeuvre
time
Manoeuvre
time
Line of Communication
Mode Imaging
Change Detection
Mode Imaging
In-theatre Control Mode Imaging
High satellite agility enables a range of responsive modes of operation
NovaSAR S-band radar mission
 SSTL Platform, 500kg satellite
 Airbus SAR S-band Payload
 Co-located AIS receiver
 400 km swath mode for maritime
 Up to 3-metre resolution
 Uses: Maritime surveillance,
deforestation, & flood monitoring
6m resolution, forest6m resolution, Pembroke docks
On Board Processing
• Advanced on-board processing
– To route communications traffic, and also
to process future surveillance satellite data,
will increase capacity, improve cueing, and
allow future systems to provide far greater
capabilities
– On-orbit configurability of sensors
– Software Defined Radios (e.g. AIS, ADS-B,
M2M communications etc)
– Image processing
• Advanced ground processing
– Cloud processing, to permit the use of
lower cost spacecraft, optics and sensors
– Compensate for spacecraft imperfections
Urthecast
• Synergistic surveillance concept
• Eight pairs of satellites
• Each pair consists of one SAR
and one optical satellite
• SAR carries AIS and a cloud sensor
• Inter-satellite link allows SAR to cue
optical satellite to avoid clouds
Mothership Concept
• An experimental mission potentially including:-
• A primary satellite with a mass of approximately 150kg
• A secondary cube-sat satellite with a mass of approximately
5kg
• Both satellites would be equipped with an attitude control
capability and the larger with an orbital manoeuvring capability
• The satellites would have an intersatellite communication link
Space Wide Web
• Optical inter-satellite links
can potentially offer both
much higher capacity and
greater communications
security than RF systems
European Data
Relay Satellite
Optical ISL Concept
• Long range ISL systems
permit commanding and
data reception from LEO
spacecraft at any time
Improved Space Situation Awareness
13
• Improvements to space situation awareness could include:-
– The tracking of smaller objects, (down to 1 cm in size)
– More frequent and more precise tracking in order to
maintain more accurate orbits
– Assessments of hostile satellite configuration,
operational status and current activity
– Warning of space weather events
• Tracking from orbit addresses several of these issues
• Launch detection from orbit is also a key capability
• A variety of technologies, including Mass drivers;
Adhesives; Harpoons; Lasers; Tethers; Nets;
Grapplers; Propulsion plumes; Slingsats; and De-
orbit sails have been suggested to remove large,
long-lived debris objects
• All these concepts are technically immature and
look like anti-satellite weapons in the wrong
hands
• It’s unclear how these concepts would be
financed, and the politics is hard too
Harpoon concept
Grappler
concept
Net concept
Mass driver concept
Adhesive concept
Slingsat concept
Propulsion plume concept
De-orbit sail concept
Tether concept
Debris Removal
Laser concept
Remove Debris Project
• SSTL is contributing to an ESA programme that
aims to test net and harpoon technology in orbit
• The remove debris mission will release two test
targets and then seek to re-capture them
Satellite Servicing Concept
• SSTL is currently working on a satellite servicing concept that is
designed to attach itself to the launch separation ring on the target
satellite
• Launched alongside a future GEO satellite, it could offer a variety of
different mission options
Assembly On Orbit
• Docking and rendezvous
technology will allow the assembly
of larger apertures on orbit
• Multiple linked mirror segments
could allow significantly improved
resolution
• These large apertures could be
used for both Earth observation and
astronomy
Space Debris As Fuel
• A team in Australia is developing a
thruster that works by ionising metals (and
carbon) and accelerating them
• Mass-drivers have also been suggested,
which can utilise almost any type of debris
• In such a scenario, space debris becomes
an on-orbit resource
• Space Traffic Control (STC) data on the
location of suitable pieces of debris
suddenly increases in value
Electric propulsion concept
Mass-driver concept
Thank You

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Dr Stuart Eves

  • 1. Innovations in Small Satellites and On-Orbit Manufacturing
  • 4. Video from Low Earth Orbit • Historically, providing video from space has been tricky:- – Having enough satellite or sensor agility to keep a single location in view for the duration of a short pass (5-10 mins) has been challenging – Spatial resolution has been low – The data rates generated by the camera have posed issues for on-board storage, data downlink, or both – Availability of ground stations for real-time control has been a problem • But video from space is coming, enabled by improved bus technologies
  • 5. The Carbonite Programme Carbonite ‘s current capability • Low-cost, high-resolution rapid response experimental EO mission • Mass = 80kg • Colour high definition video • Direct delivery to users • Designed and built in 7 months • Carbonite-2 under construction (1-metre resolution – post-processed to 0.5-metre) Carbonite ‘s future iterations • 0.5m to 1m resolution • Full colour, stills and HD video • 1400 images per day • 450s video per day • <50kg • 3 months to launch
  • 6.
  • 7. Low-Elevation Mode Imaging Multiple Imagery Collection Modes Highly Agile Single Scene Imaging Extended Strip Imaging In-pass Stereo Mode Imaging Area Mode Imaging 12 Super-Resolution Mode Imaging Strip 1 Strip 2 Strip 3 Strip 4 Manoeuvre time Manoeuvre time Manoeuvre time Line of Communication Mode Imaging Change Detection Mode Imaging In-theatre Control Mode Imaging High satellite agility enables a range of responsive modes of operation
  • 8. NovaSAR S-band radar mission  SSTL Platform, 500kg satellite  Airbus SAR S-band Payload  Co-located AIS receiver  400 km swath mode for maritime  Up to 3-metre resolution  Uses: Maritime surveillance, deforestation, & flood monitoring 6m resolution, forest6m resolution, Pembroke docks
  • 9. On Board Processing • Advanced on-board processing – To route communications traffic, and also to process future surveillance satellite data, will increase capacity, improve cueing, and allow future systems to provide far greater capabilities – On-orbit configurability of sensors – Software Defined Radios (e.g. AIS, ADS-B, M2M communications etc) – Image processing • Advanced ground processing – Cloud processing, to permit the use of lower cost spacecraft, optics and sensors – Compensate for spacecraft imperfections
  • 10. Urthecast • Synergistic surveillance concept • Eight pairs of satellites • Each pair consists of one SAR and one optical satellite • SAR carries AIS and a cloud sensor • Inter-satellite link allows SAR to cue optical satellite to avoid clouds
  • 11. Mothership Concept • An experimental mission potentially including:- • A primary satellite with a mass of approximately 150kg • A secondary cube-sat satellite with a mass of approximately 5kg • Both satellites would be equipped with an attitude control capability and the larger with an orbital manoeuvring capability • The satellites would have an intersatellite communication link
  • 12. Space Wide Web • Optical inter-satellite links can potentially offer both much higher capacity and greater communications security than RF systems European Data Relay Satellite Optical ISL Concept • Long range ISL systems permit commanding and data reception from LEO spacecraft at any time
  • 13. Improved Space Situation Awareness 13 • Improvements to space situation awareness could include:- – The tracking of smaller objects, (down to 1 cm in size) – More frequent and more precise tracking in order to maintain more accurate orbits – Assessments of hostile satellite configuration, operational status and current activity – Warning of space weather events • Tracking from orbit addresses several of these issues • Launch detection from orbit is also a key capability
  • 14. • A variety of technologies, including Mass drivers; Adhesives; Harpoons; Lasers; Tethers; Nets; Grapplers; Propulsion plumes; Slingsats; and De- orbit sails have been suggested to remove large, long-lived debris objects • All these concepts are technically immature and look like anti-satellite weapons in the wrong hands • It’s unclear how these concepts would be financed, and the politics is hard too Harpoon concept Grappler concept Net concept Mass driver concept Adhesive concept Slingsat concept Propulsion plume concept De-orbit sail concept Tether concept Debris Removal Laser concept
  • 15. Remove Debris Project • SSTL is contributing to an ESA programme that aims to test net and harpoon technology in orbit • The remove debris mission will release two test targets and then seek to re-capture them
  • 16. Satellite Servicing Concept • SSTL is currently working on a satellite servicing concept that is designed to attach itself to the launch separation ring on the target satellite • Launched alongside a future GEO satellite, it could offer a variety of different mission options
  • 17. Assembly On Orbit • Docking and rendezvous technology will allow the assembly of larger apertures on orbit • Multiple linked mirror segments could allow significantly improved resolution • These large apertures could be used for both Earth observation and astronomy
  • 18. Space Debris As Fuel • A team in Australia is developing a thruster that works by ionising metals (and carbon) and accelerating them • Mass-drivers have also been suggested, which can utilise almost any type of debris • In such a scenario, space debris becomes an on-orbit resource • Space Traffic Control (STC) data on the location of suitable pieces of debris suddenly increases in value Electric propulsion concept Mass-driver concept