Transcript Slide 1

There is always Space for
Quality
Dr Mark English
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Space and Software
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Cassini / Huygens – the plan
3.5 Billion kms
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Cassini/Huygens
Mariner MKII spacecraft
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Source: NASA
Cassini
Mariner MKII
spacecraft
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Source: NASA
Cassini/Huygens Flight Model
Mariner MKII
spacecraft
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The Surface Science Package
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Source: John Zarnecki, PSSRI, Open University, UK
Cassini / Huygens – the plan
3.5 Billion kms
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Titan
Titan’s vital statistics:
Diameter – 5150km; Orbital/rotational period – 15.95 days
Only planetary satellite with atmosphere
Column mass ~ 10 x value for Earth
Atmospheric Composition
Nitrogen and rich array of hydrocarbons and nitriles
Hidden Surface
Obscured by photochemical haze
Indirect evidence for surface seas/lakes
Model for early Earth?
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Overall model of Titan
Source: R. Lorenz
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Considerations
Delivery mechanisms
Target environment
Transition environment
Duration of operation
Nature of operation
Sound familiar?
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Design and Build
Look at key facts – with tolerance
Temperature
Vacuum
Radiation
Time
Chemistry
Zero gravity
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The Mission
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Survival
Launch – shaking (a lot)
Cruise – radiation & vacuum
Cruise – thermal control
Cruise – temperature cycling
Trajectory and SOI – accuracy
Entry & Surface mission - cold
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Launch
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Getting through Launch
Make it ... then shake it
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Cruise
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The flight plan
VVEJGA
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Source: NASA
The flight plan
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Source: BBC
Temperature Control
Gets cold out there
No solar panels for electric heating
Too far, sun too weak
Too much dust
Use RTGs for power
Use RHUs for on-platform heat
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Keeping warm
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Keeping warm
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Radiation
Sources
Natural (Sun, Cosmic)
RTGs
RHUs
Total dose to outside of shield
24.15 kRads
Qual level ... double it
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Proven technology
No Moving parts
No lubricant
Solid actuators
No normal solder
Crystallisation
Outgassed plastics
No nasty condensation
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Proven technology
Radhard ICs
Care with Digital and analogue lines
Waiver and qualification for E2PROMS
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You can never go back Dorothy
Once it is launched there is no
maintenance ...
It has to work first time, the first time...
How do you get to this level of quality?
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Systems engineering
Developed through Minuteman,
Used on Apollo
Working to interfaces, and
specifications
Big design, modular breakdown
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Modules
See this in Software ...
Code libraries (NAG)
Component based development
Requires very strict library
management and definition
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Libraries
Numerical Algorithms Group
http://www.nag.co.uk/
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Libraries
Not enough to know what things do
How were they tested?
What tolerances were on that data?
What operational environment?
What Units?
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Failures
Mars has swallowed 12 missions
Mars observer 1993
Mars global surveyor 1996
Mars climate orbiter 1999
Ariane 5 1996
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Caveat
Any well meaning highly skilled
operator can try and do
something and screw it up like
any of us
You get this in all industries.
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Cassini / Huygens – the plan
3.5 Billion kms
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SOI
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Arriving at Saturn
Saturn Orbit Insertion
Turned spacecraft round
Fired motors for 96 Minutes
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Source: Huygens Mission Operations Plan
Arriving at Saturn
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Source: Huygens Mission Operations Plan
Ejection
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How Cassini supports Huygens
Radio uplink during mission using HGA
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Source: NASA
Atmospheric Entry and Surface
Mission
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Any other risks?
Hm......
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Atmospheric Models
Yelle et al. 1997
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Huygens descent timelines
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Source: John Zarnecki, PSSRI, Open University, UK / ESA
Parachute Test
A test drop was done on Earth
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Source: ESA
SSP
Measure:
Temperature
Speed of sound
Acceleration
Refractive properties
Liquid Density
Thermal Properties
Electrical Properties
Angle of tilt
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Source: PSSRI
SSP
Measure:
Temperature
Speed of sound
Acceleration
Refractive properties
Liquid Density
Thermal Properties
Electrical Properties
Angle of tilt
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Source: PSSRI
Shake and Bake (!)
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Source: John Zarnecki, PSSRI, Open University, UK
Prepare the spacecraft
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Cassini
Mariner MKII
spacecraft
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Source: NASA
Design Constraints
Survive Launch
Very high G shock
Radiation proof (Rad hard)
Solar radiation
RHUs and RTGs
Reliable over 7 years cruise
Vacuum
Zero gravity
Reliable during 69 orbits
Surface mission
Atmospheric entry
Cryogenic cooling (-200 degC)
Dunking into Liquid Ethane/Methane mix
Manufactured in 1994
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Qualification
Launch
Calculate the resonant frequencies
Shake it on a test bed
Radiation proof (Rad hard)
Irradiate all components
Reliable over 7 years cruise
Bake out all volatiles
Reliable during 69 orbits (!)
Surface mission
Cryogenic cooling (-200 degC)
Dunking into Liquid Ethane/Methane mix
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Project Management
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Documentation
ISO 9000, BS5750
Fully documented
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Documentation
ISO 9000, BS5750
Each operation mapped out
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The results
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The Landing Site
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Source: ESA
Descent to Titan - Surface mode
Dull thud
Major Instruments:
SSP
DISR
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Surface View
Titan surface
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Credits: ESA/NASA/JPL/University of Arizona
DISR – Panorama
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Summary
Exploration
A lot of engineering
A lot of planning
A lot of people
Science objectives, Risk driven development
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Source: NASA
Acknowledgements
PSSRI of the Open University, UK
Access to Huygens datastore
Mark Leese, SSP programme manager
NASA
ESA
Proxima Ltd.
Ralph Lorenz, LPL, Univ. Arizona
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Resources
European Space Agency
http://sci.esa.int/Huygens
National Aeronautics and Space Administration
http://saturn.jpl.nasa.gov
Planetary and Space Science Research Institute
http://pssri.open.ac.uk/missions/mis-casa.htm
Zen, and the art of motorcycle maintenance, Robert Pirsig
The New Solar System, J. Kelly Beatty and Andrew Chaikin
(eds), Sky Publications.
Software Engineering Standards, Mazza et. al., Prentice
Hall
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