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Slide 1 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 The Cassini-Huygens Mission to Saturn and Titan Professor John C. Zarnecki.

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Presentation on theme: "Slide 1 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 The Cassini-Huygens Mission to Saturn and Titan Professor John C. Zarnecki."— Presentation transcript:

1 Slide 1 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 The Cassini-Huygens Mission to Saturn and Titan Professor John C. Zarnecki

2 Slide 2 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 Saturn and Titan

3 Slide 3 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 Saturn  Most distant planet visible with the naked eye  2 nd largest planet in the solar system  Gas giant – primarily Hydrogen and Helium  34 known moons at present  1.5 billion km mean distance from the sun, 10 x more distant than the Earth  Unique complex ring system

4 Slide 4 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 Titan  Saturn’s largest moon  Discovered by Christiaan Huygens in 1655  Diameter of 5150 km  Atmospheric pressure of 1.5 bar  Surface temperature ~ 96 K (-177°C)

5 Slide 5 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 Why Titan?  Only planetary satellite with atmosphere (column mass ~ 10 x value for Earth)  Surface – obscured by photochemical haze  Atmosphere – mainly N 2 with CH 4 and an array of hydrocarbons and nitriles  Indirect evidence for surface seas/lakes (i.e. a methane ‘source’)  A ‘primordial atmosphere’ (but frozen!) → an ancient earth?

6 Slide 6 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 The Cassini/Huygens Mission

7 Slide 7 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 The Cassini Spacecraft  Joint ESA/NASA mission  Launched 15 th October 1997  6.7 m high  2125 kg at launch  After a 7 year (4 billion km) journey, Cassini arrived at Saturn in July 2004.

8 Slide 8 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 The Gravity Assist Trajectory

9 Slide 9 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 Saturn Orbit Insertion

10 Slide 10 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 The Huygens Probe  Determine atmospheric composition  Study aerosol properties and cloud physics  Characterise the upper atmosphere  Imaging the surface for the first time  Determine the physical properties of the surface material

11 Slide 11 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 Industry  LogicaCMG – Mission critical on-board software, including Probe control software, Cassini/Huygens communications relay software and in flight software maintenance.  Martin Baker Space Systems – Parachute systems and related structural components, mechanisms and pyrotechnics.  Irvin Aerospace – Sub-contractor to Martin Baker responsible for definition of each of the three disk gap band parachutes.  IGG Component Technology - Centralised procurement and testing of electrical, electronic and electromechanical components.  SciSys – Mission control system development and operational support.

12 Slide 12 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 List of Instruments 1.Huygens Atmospheric Structure Instrument (HASI) Fulchignoni, Paris, France. 2.Gas Chromatograph Mass Spectrometer (GCMS) Niemann, NASA, USA 3.Aerosol Collector and Pyrolyser (ACP) Israel, CNRS, France. 4.Descent Imager/Spectral Radiometer (DISR) Tomasko, Arizona, USA 5.Doppler Wind Experiment (DWE) Bird, Bonn, USA 6.Surface Science Package (SSP) Zarnecki, OU, UK.

13 Slide 13 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005

14 Slide 14 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 The Surface Science Package (SSP)

15 Slide 15 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 SSP Flight Integration

16 Slide 16 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 SSP Sensor Description

17 Slide 17 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 Selected Properties Measured by SSP

18 Slide 18 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 ATMOSPHERE SOLID MUD LIQUID

19 Slide 19 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 ACC-I (Internal Accelerometer)  Piezoelectric accelerometer  Max ~100 g detection  Impact dynamics measurement (deceleration)

20 Slide 20 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 ACC-E (Penetrometer)  Piezoelectric force transducer  Protrudes from probe base  First instrument to touch Titan’s surface  Impact measurement of penetration through the surface layer (mechanical properties of the surface)

21 Slide 21 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 TIL (Probe Attitude)  Measures tilt relative to 1 axis  Electrolytic liquid in a glass vial  Fluid movement relative to electrodes → tilt angle

22 Slide 22 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 API-V (Speed of Sound)  2 piezoelectric transducers generate ultrasonic pulse  Alternate T x /R x mode  Arranged facing each other  Time taken for pulse to be detected → speed of sound in the Titan atmosphere (molecular mass)

23 Slide 23 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 API-S (Sounder)  10 resonant piezoelectric plates  Simultaneously form a 20° acoustic beam  Orientated towards the surface  Surface profile echoes  Ocean/lake sounder

24 Slide 24 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 THP (Thermal Properties)  Thin wire technique  50 µm Pt wire pulsed with high current  R Ω (t) measured  Thermal conductivity derived (gas mixture components)

25 Slide 25 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 DEN (Density)  Archimedes’ principle  Float suspended in chamber  Buoyancy in immersed liquid measured by strain gauges → density

26 Slide 26 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 REF (Refractometer)  Critical angle refractometer  Linear photodiode array and specially designed prism  Refractive index of immersed liquid measured (light-dark transition)

27 Slide 27 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 PER (Permittivity and Conductivity)  Stacked parallel plates  Capacitance measured  Permittivity and conductivity of the liquid measured

28 Slide 28 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 Landing On Titan

29 Slide 29 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 Arrival and Descent

30 Slide 30 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 Possible Landing Scenarios

31 Slide 31 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 High Altitude Images Altitude 16.2 km, 40m per pixel resolution Credits: ESA/NASA/University of Arizona Altitude 8 km, 20m per pixel resolution

32 Slide 32 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 High Altitude Images Credits: ESA/NASA/University of Arizona Altitude 16.2 km, 40 m per pixel resolution

33 Slide 33 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 A View from 10 km Credits: ESA/NASA/University of Arizona

34 Slide 34 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 Views at the surface Credits: ESA/NASA/University of Arizona

35 Slide 35 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 The Impact on the Surface

36 Slide 36 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 The Impact on the Surface

37 Slide 37 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 Impact Simulations Over 100 vertical and oblique drops into 16 different substrate materials. Coarse GravelSand SiliBeads Crème BruleeDrop Test Rig

38 Slide 38 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 Impact Simulations

39 Slide 39 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 Impact Simulations

40 Slide 40 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 Impact Dynamics – First Look ACC-I (deceleration): 35ms deceleration pulse, peak 15g – Huygens probe decelerated over circa 16cm; Model comparison suggests material with uniform strength vs. depth, ~10 N cm -2 ACC-E (penetration force): 50N resistance with some variation – possibly a pebble strike, possible sub-surface granular structure on cm scale or finer

41 Slide 41 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 API-S Surface Detection

42 Slide 42 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 API-V Speed of sound increases with temperature at lower altitude

43 Slide 43 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 SSP Data Summary SSP has received ALL of its Science Data via Channel B. All SSP sensors have given the expected output for the atmospheric and surface conditions encountered. We have data up to T0 + 13,046secs (3hrs, 37mins, 26secs). Data from surface for 1hr, 9 mins, 36secs

44 Slide 44 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 17 January 2005L.Gurvits and the Huygens VLBI Tracking Team Doppler (wind and more….) measurements Huygens carrier at Green Bank, Mk5 VLBI

45 Slide 45 of 45 Prof. John ZarneckiRAeS – 22 nd March 2005 Acknowledgements SSP Science Team Huygens Science Team ESA NASA Polish Academy of Sciences University of Manchester Rutherford Appleton Laboratory Particle Physics and Astronomy Research Council


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