using speed of sound measurements to constrain the huygens probe descent profile

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Planetary Probe Atmospher ic Entry Workshop, Lisbon , 6-9 October 2003 1 ILEWG Using speed of sound measurements to constrain the Huygens Probe descent profile H. Svedhem, J-P. Lebreton ESA/RSSD, NL J. Zarnecki, B. Hati Open University, UK

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Using speed of sound measurements to constrain the Huygens Probe descent profile. H. Svedhem, J-P. Lebreton ESA/RSSD, NL J. Zarnecki, B. Hati Open University, UK. John Tyndall’s atmospheric experiment 1875. - PowerPoint PPT Presentation

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Page 1: Using speed of sound measurements to constrain the Huygens Probe descent profile

Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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Using speed of sound measurements to constrain the Huygens Probe descent profile

H. Svedhem, J-P. LebretonESA/RSSD, NL

J. Zarnecki, B. HatiOpen University, UK

Page 2: Using speed of sound measurements to constrain the Huygens Probe descent profile

Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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ILEWGJohn Tyndall’s atmospheric

experiment 1875

Page 3: Using speed of sound measurements to constrain the Huygens Probe descent profile

Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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About 100 years later Jean-Pierre Lebreton proposes to fly an acoustic sensor to Titan

• We now talk about miniaturisation…..

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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The Acoustic Properties Investigation (API) of the Surface Science Package on Huygens

• API has two sets of sensors and one card of electronics incorporated in to the SSP Top Hat and electronics box– API-S, (sounder) is a monostatic SODAR for detection of

atmospheric precipitation during the descent, surface characterisation during the last phase of the descent and detection of sea depth in case of landing in a liquid.

– API-V, (velocity) will measure the speed of sound across a 15 cm long path during the descent from an altitude of about 50 km down to the surface, and in the liquid in case of landing in a liquid.

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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API-S

• The API-S in principle works as a conventional SODAR.• The return signal is proportional to the number density of

the scattering particles in the scattering volume and to the particle diameter to the 6th power. (Rayleigh scattering)

• For both volume scattering and surface scattering the signal is inversely proportional to the square of the distance.

• The similarities to Radars are striking. By coincidence the wavelength of the API-S and the probe altimeter are both about 2 cm. Comparisons will be useful.

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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API-S Modes 1/2

• Atmospheric sounding mode, >7km. Search for hydrometeors and turbulence. Pulse length 10 ms. Binned samples for the closes 50 m are stored each 2 seconds.

• Surface proximity mode,7km>h>1km. Pulse length 10 ms. Search for surface return AND hydrometeors. Binned samples at higher resolution around the surface bin each 3 seconds.

• Near surface mode. h<1km. Pulse length 2 ms. Search for surface structure and topography. Binned samples at highest resolution around the surface bin each second.

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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API-S Modes 2/2

• Surface mode. After impact, search for depth of liquid. Pulse length 10 ms. Send one pulse, listen for 10 s. Binned data around the maximum return.

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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API-V mode

• One mode only at h<60 km. Sensor A transmits a pulse and start a 4 Mhz counter, sensor B receives the pulse and stops the counter. Immediately afterwards the sequence is repeated in the reverse direction. Both data are stored. Frequency of measurement is 1 s.

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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API-S reflectivity factors, Z

Hydrometeor condition Precipitation rate Z[mm/h] [mm6m-3]

Cloud 0.001 to 1Fog 0.01 to 1Drizzle 1 10Light Rain 1 200Heavy Rain 25 33000Light Snow 1 1000Heavy Snow 10 40000

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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API-S Performance

-40

-30

-20

-10

0

10

20

30

0 0.5 1 1.5 2 2.5 3 3.5 4 4.5

log Z [mm6m-3]

Echo

leve

l [dB

, ref

20

uPa]

d=50 md=10 mNoise level

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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Performance API-S

• Reflectivity factors on earth are known, (previous graph). Titan situation is hard to estimate.

• Garry (1996)estimated, based on data from Toon et al (1988) that the reflectivity factors at Titan are too low to be detected by API-S. The method for these calculations was however unconventional and seem to give too pessimistic results.

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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API-V pressure sensitivity

0.01

0.1

1

10

100

0 200 400 600 800 1000 1200 1400

Pressure [mBar]

Rec

eive

r out

put [

mV]

N=10N=1

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Error analysis

• M = ·R · T · c-2

M/M=((T/T)2+ (2c/c)2)1/2

• For the gasses at the temperatures we have c is about 200 m/s, we get with 250 ns resolution and 15 cm path, 2c/c 7 ·10-4. T 0.1 K which at 100 K gives T/T = 10-3. The contributions are thus of the same order of magnitude.

M/M 1.2 ·10-3 .

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Empirical approach, gas

• In stead of calculating the mean molecular weigh one may go directly to find mixing ratios from calibrated measurements.

• The mixing ratio will be accurate to better than 1 % for binary gasses. The number is dependent on which species are involved.

• This will work well for binary mixtures but is difficult for mixtures of three or more gasses (or liquids)

• For mixtures of three or more components a test of the expected sound speed can give useful constraints to measurements by other instruments.

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Empirical approach, liquid

• For the liquids the sound speeds are typically ten times higher while the resolution remains 250 ns. Hence the c/c is the dominating error.

• The spread in sound speed is larger and therefore a precision in the mixing ratio similar to that of gasses will be achieved, i.e. about 1% for binary mixtures.

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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API-V in Nitrogen gas

150

170

190

210

230

250

270

290

310

-190 -170 -150 -130 -110 -90 -70 -50Temperature [deg C]

Soun

d sp

eed

[m/s

]

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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API-V in 100% Methane gas

200

250

300

350

400

450

500

-200 -150 -100 -50 0 50Temperature [deg C]

Soun

d sp

eed

[m/s

]

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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API-V in 100% Ethane gas

245

250

255

260

265

270

275

280

285

290

-100 -80 -60 -40 -20 0Temperature [deg C]

Soun

d sp

eed

[m/s

]

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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API-V in 100% Ethane liquid

1100

1300

1500

1700

1900

2100

-190 -170 -150 -130 -110 -90 -70 -50Temperature [deg C]

Soun

d sp

eed

[m/s

]

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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API-V in 100% Methane liquid

1320

1340

1360

1380

1400

1420

1440

1460

1480

1500

-180 -175 -170 -165 -160Temperature [deg C]

Soud

spe

ed [m

/s]

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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What about the miniaturisation, did it work

out?

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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Planetary Probe Atmospheric Entry Workshop, Lisbon, 6-9 October 2003

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