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There is always Space for Quality. Dr Mark English. Space and Software. Cassini / Huygens – the plan. 3.5 Billion kms. Cassini/Huygens. Mariner MKII spacecraft. Source: NASA. Cassini. Mariner MKII spacecraft. Source: NASA. Cassini/Huygens Flight Model. Mariner MKII spacecraft.
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There is always Space for Quality Dr Mark English
Cassini / Huygens – the plan 3.5 Billion kms
Cassini/Huygens Mariner MKII spacecraft Source: NASA
Cassini Mariner MKII spacecraft Source: NASA
Cassini/Huygens Flight Model Mariner MKII spacecraft
The Surface Science Package Source: John Zarnecki, PSSRI, Open University, UK
Cassini / Huygens – the plan 3.5 Billion kms
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?
Overall model of Titan Source: R. Lorenz
Considerations Delivery mechanisms Target environment Transition environment Duration of operation Nature of operation Sound familiar?
Design and Build Look at key facts – with tolerance Temperature Vacuum Radiation Time Chemistry Zero gravity
Survival Launch – shaking (a lot) Cruise – radiation & vacuum Cruise – thermal control Cruise – temperature cycling Trajectory and SOI – accuracy Entry & Surface mission - cold
Getting through Launch Make it ... then shake it
The flight plan VVEJGA Source: NASA
The flight plan 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
Radiation Sources Natural (Sun, Cosmic) RTGs RHUs Total dose to outside of shield 24.15 kRads Qual level ... double it
Proven technology No Moving parts No lubricant Solid actuators No normal solder Crystallisation Outgassed plastics No nasty condensation
Proven technology Radhard ICs Care with Digital and analogue lines Waiver and qualification for E2PROMS
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?
Systems engineering Developed through Minuteman, Used on Apollo Working to interfaces, and specifications Big design, modular breakdown
Modules See this in Software ... Code libraries (NAG) Component based development Requires very strict library management and definition
Libraries Numerical Algorithms Group http://www.nag.co.uk/
Libraries Not enough to know what things do How were they tested? What tolerances were on that data? What operational environment? What Units?
Failures Mars has swallowed 12 missions Mars observer 1993 Mars global surveyor 1996 Mars climate orbiter 1999 Ariane 5 1996
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.
Cassini / Huygens – the plan 3.5 Billion kms
Arriving at Saturn Saturn Orbit Insertion Turned spacecraft round Fired motors for 96 Minutes Source: Huygens Mission Operations Plan
Arriving at Saturn Source: Huygens Mission Operations Plan
How Cassini supports Huygens Radio uplink during mission using HGA Source: NASA
Any other risks? Hm......
Atmospheric Models Yelle et al. 1997
Huygens descent timelines Source: John Zarnecki, PSSRI, Open University, UK / ESA
Parachute Test A test drop was done on Earth Source: ESA
SSP Measure: Temperature Speed of sound Acceleration Refractive properties Liquid Density Thermal Properties Electrical Properties Angle of tilt Source: PSSRI
SSP Measure: Temperature Speed of sound Acceleration Refractive properties Liquid Density Thermal Properties Electrical Properties Angle of tilt Source: PSSRI
Shake and Bake (!) Source: John Zarnecki, PSSRI, Open University, UK
Cassini Mariner MKII spacecraft 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