The Huygens probe, supplied by the European Space Agency (ESA)
and named after the Dutch 17th century astronomer Christiaan Huygens, is an
atmospheric entry probe and lander carried to Saturn's moon Titan as part of the Cassini-Huygens mission. The combined
Cassini-Huygens spacecraft was launched from Earth on October 15, 1997. Huygens separated from the Cassini orbiter on
December 25, 2004, and landed on Titan on January 14, 2005 near the Xanadu
region. It touched down on land, although the possibility that it would touch down in an ocean was also taken into account in its
design. The probe continued to send data for about 90 minutes after reaching the surface.
Overview
Huygens was designed to enter and brake in Titan's atmosphere and parachute a fully instrumented robotic laboratory
down to the surface. When the mission was planned, it was not yet certain whether the landing site would be a mountain range, a flat plain, an ocean, or
something else, and it was hoped that analysis of data from Cassini would help to answer these questions.
The first image released, taken from an altitude of 16 km, showing what are speculated to be drainage channels flowing to a
possible shoreline. The darker areas are flat plains, while the lighter areas represent high ground.
Based on pictures taken by Cassini at 1,200 km away from Titan, the landing site appeared to be, for want of a better
word, shoreline. Assuming the landing site could be non-solid, the Huygens probe was designed to survive the impact and
splash-down with Titan's liquid surface for several minutes and send back data on the conditions there. If that occurred it was
expected to be the first time a human-made probe would land in an extraterrestrial (i.e. non-Earth) ocean. The spacecraft had no
more than three hours of battery life, most of which was planned to be taken up by the descent. Engineers only expected to get at
best 30 minutes of data from the surface.
The Huygens probe system consists of the 318 kg probe itself, which descended to Titan, and the probe support equipment
(PSE), which remained attached to the orbiting spacecraft. Huygens' heat shield was 2.7 m in diameter; after ejecting the shield,
the probe was 1.3 m in diameter. The PSE included the electronics necessary to track the probe, to recover the data gathered
during its descent, and to process and deliver the data to the orbiter, from which it will be transmitted or "downlinked" to the
ground.
The probe remained dormant throughout the 6.7-year interplanetary cruise, except for bi-annual health checks. These checkouts
followed preprogrammed descent scenario sequences as closely as possible, and the results were relayed to Earth for examination
by system and payload experts.
Prior to the probe's separation from the orbiter on December 25 2004, a final health check was performed. The "coast" timer was loaded with the precise time necessary to turn on
the probe systems (15 minutes before its encounter with Titan's atmosphere), then the probe detached from the orbiter and coasted
in free space to Titan in 22 days with no systems active except for its wake-up timer.
The main mission phase was a parachute descent through Titan's atmosphere. The batteries and all other resources were sized
for a Huygens mission duration of 153 minutes, corresponding to a maximum descent time of 2.5 hours plus at least 3
additional minutes (and possibly a half hour or more) on Titan's surface. The probe's radio link was activated early in the
descent phase, and the orbiter "listened" to the probe for the next 3 hours, including the descent phase, and the first thirty
minutes after touchdown. Not long after the end of this three-hour communication window, Cassini's high-gain antenna (HGA)
was turned away from Titan and toward Earth.
Very large radio telescopes on Earth were also listening to Huygens's 10-watt transmission using the technique of
very long baseline interferometry and aperture synthesis mode. At
11:25 CET on January 14, the Robert C. Byrd Green Bank Telescope (GBT) in West
Virginia detected the carrier signal from the Huygens probe. The GBT continued to detect the carrier signal well after
Cassini stopped listening to the incoming data stream. In addition to the GBT, eight of the ten telescopes of the
continent-wide VLBA in North America, located at Pie Town and Los Alamos, NM; Fort Davis, TX; North Liberty, IA; Kitt Peak, AZ;
Brewster, WA; Owens Valley, CA; and
Mauna Kea, HI, also listened for the Huygens signal.
The signal strength received at Earth from Huygens was comparable to that from the Galileo probe (the Jupiter atmospheric descent probe) as received by the VLA, and was therefore too weak to detect in real time because of the signal modulation by the (then)
unknown telemetry. Instead, wide-band recordings of the probe signal were made throughout the
three-hour descent. After the probe telemetry was finished being relayed from Cassini to Earth, the recorded signal was
processed against a telemetry template, enabling signal integration over several seconds for determining the probe frequency. It
was expected that through analysis of the Doppler shifting of Huygens' signal as it descended through the atmosphere of
Titan, wind speed and direction could be determined with some degree of accuracy. Through interferometry, it was also expected
that the radio telescopes would allow determination of Huygens's landing site on Titan with exquisite precision, measuring
its position to within 1 km at a distance from Earth of about 1200 million kilometres). This
represents an angular resolution of approximately 170 microarcseconds. A similar technique was used to determine the landing site of the Mars exploration rovers by listening to their telemetry alone.
Findings
Huygens landing site as determined by descent imagery
Preliminary findings seemed to confirm the presence of large bodies of liquid on the surface of Titan. The photos showed what
appear to be large drainage channels crossing the lighter colored mainland into a dark sea. Some of the photos even seem to
suggest islands and mist shrouded coastline.
At the landing site there were indications of chunks of water ice scattered over an orange surface, the majority of which is
covered by a thin haze of methane. The instruments revealed "a dense cloud or thick haze
approximately 18-20 kilometers from the surface". The surface itself was reported to be a clay-like
"material which might have a thin crust followed by a region of relative uniform consistency." One ESA scientist compared the
texture and color of Titan's surface to a Crème brûlée, but admitted this term probably
would not appear in the published papers.
On January 18 it was reported that Huygens landed in "Titanian mud", and the
landing site was estimated to lie within the white circle on the picture to the right. Mission scientists also reported a first
"descent profile", which describes the trajectory the probe took during its descent.
However, subsequent analysis of the data suggests that surface consistency readings were likely caused by Huygens
displacing a large pebble as it landed, and that the surface is better described as a 'sand' made of ice grains.[1] The images taken after the probe's landing show a flat plain
covered in pebbles. The pebbles, which may be made of water ice, are somewhat rounded, which may indicate the action of fluids on
them.[2]
Further work done on the probe's trajectory indicate that in fact it landed within the dark 'sea' region in the photos. Photos
of a dry landscape from the surface contradict the original theory that the dark regions were liquid seas, leading researchers to
conclude that while there was evidence of liquid acting on the surface recently, the much anticipated hydrocarbon seas of Titan
were in fact absent.
Detailed Huygens activity timeline
Ellipse shows approximate landing site on this image taken earlier by
Cassini. The bright region to the right is
Xanadu Regio.
Coloured image released from the landing site.
Contrast-enhanced version of surface image
- Huygens probe separated from Cassini orbiter at 02:00 UTC
on December 25, 2004 in Spacecraft Event Time.
- Huygens probe entered Titan's atmosphere at 10:13 UTC on January 14,
2005 in SCET, according to ESA.
- The probe landed on the surface of the moon at ~163.1775 degrees east and ~10.2936 degrees south around 12:43 UTC in SCET (2
hours 30 minutes after atmospheric entry).(1.)
There was a transit of the Earth and Moon across the Sun as seen from Saturn/Titan just hours before the landing. The
Huygens probe entered the upper layer of Titan's atmosphere 2.7 hours after the end of the transit of the Earth, or only
one or two minutes after the end of the transit of the Moon. However, the transit did not interfere with Cassini orbiter
or Huygens probe, for two reasons. First, although they could not receive any signal from Earth because it was in front of
the Sun, Earth could still listen to them. Second, Huygens did not send any readable data to the Earth; it transmitted
data to Cassini orbiter, which relayed the data received to the Earth later. For details about transits of the Earth as
seen from Saturn, see also Transit of Earth from Saturn.
See also Detailed timeline of Huygens mission.
Instrumentation
The Huygens probe had six complex instruments aboard that took in a wide range of scientific data after the probe
descended into Titan's atmosphere. The six instruments are:
Huygens Atmospheric Structure Instrument (HASI)
This instrument contains a suite of sensors that measured the physical and electrical properties of Titan's atmosphere.
Accelerometers measured forces in all three axes as the probe descended through the
atmosphere. With the aerodynamic properties of the probe already known, it was possible to determine the density of Titan's
atmosphere and to detect wind gusts. The probe was designed so that in the event of a landing on a liquid surface, its motion due
to waves would also have been measurable. Temperature and pressure sensors measured the thermal properties of the atmosphere. The
Permittivity and Electromagnetic Wave Analyzer component measured the electron and
ion (i.e., positively charged particle) conductivities of the atmosphere and searched for
electromagnetic wave activity. On the surface of Titan, the conductivity and permittivity (i.e., the ratio of electric flux density produced to the strength of the electric
field producing the flux) of the surface material was measured. The HASI subsystem also contains a microphone, which was
used to record any acoustic events during probe's descent and landing; [3] this was only the second time in history that audible sounds from another planetary body had been
recorded (a Venera-13 recording being the first).
Doppler Wind Experiment (DWE)
This experiment used an ultra-stable oscillator to improve communication with the probe
by giving it a very stable carrier frequency. This instrument was also used to measure the wind speed in Titan's atmosphere by
measuring the Doppler shift in the carrier signal. The swinging motion of the probe
beneath its parachute due to atmospheric properties may also have been detected. Although the failure of one of Huygens's
data channels resulted in this data being lost to Cassini, enough was picked up by Earth-based radio telescopes to reconstruct it. Measurements started 150 kilometres above Titan's surface, where
Huygens was blown eastwards at more than 400 kilometres per hour, agreeing with earlier measurements of the winds at 200
kilometres altitude, made over the past few years using telescopes. Between 60 and 80
kilometres, Huygens was buffeted by rapidly fluctuating winds, which are thought to be vertical wind shear. At ground level, the
Earth-based doppler shift and VLBI measurements show gentle winds of a
few metres per second, roughly in line with expectations.
Descent Imager/Spectral Radiometer (DISR)
This instrument made a range of imaging and spectral observations using several sensors and fields of view. By measuring the
upward and downward flow of radiation, the radiation balance (or imbalance) of the thick Titan atmosphere was measured. Solar
sensors measured the light intensity around the Sun due to scattering by aerosols in the atmosphere. This permitted calculation of the size and number density of the suspended
particles. Two imagers (one visible, one infrared) observed the surface during the latter stages of the descent and, as the probe
slowly spun, they built up a mosaic of pictures around the landing site. In addition, a side-view visible imager obtained a
horizontal view of the horizon and of the underside of the cloud deck. For spectral measurements of the surface, a lamp was
switched on shortly before landing to augment the weak sunlight.
Gas Chromatograph Mass Spectrometer (GC/MS)
A worker in the Payload Hazardous Servicing Facility (PHSF) stands behind the bottom side of the experiment platform for the
Huygens probe.
This instrument is a versatile gas chemical analyzer that was designed to identify and measure chemicals in Titan's
atmosphere.[4] It was equipped with samplers that were
filled at high altitude for analysis. The mass spectrometer, a high-voltage
quadrupole, collected data to build a model of the molecular masses of each gas, and a more powerful separation of molecular and
isotopic species was accomplished by the gas chromatograph.[5] During descent, the GC/MS also analyzed
pyrolysis products (i.e., samples altered by heating) passed to it from the Aerosol Collector Pyrolyser. Finally, the
GC/MS measured the composition of Titan's surface. This
investigation was made possible by heating the GC/MS instrument
just prior to impact in order to vaporize the surface material upon contact. The GC/MS was developed by the Goddard Space Flight Center and University of
Michigan's Space Physics Research Lab.
Aerosol Collector and Pyrolyser (ACP)
The ACP experiment drew in aerosol particles from the atmosphere through filters, then
heated the trapped samples in ovens (using the process of pyrolysis) to vaporize
volatiles and decompose the complex organic materials. The products were flushed along a pipe
to the GC/MS instrument for analysis. Two filters were provided to
collect samples at different altitudes.[6] The ACP was
developed by a (French) ESA team at the Laboratoire Inter-Universitaire des
Systèmes Atmosphériques (LISA).
Surface-Science Package (SSP)
The SSP contained a number of sensors designed to determine the physical properties of Titan's surface at the point of impact,
whether the surface was solid or liquid. An acoustic sounder, activated during the last 100 meters
of the descent, continuously determined the distance to the surface, measuring the rate of descent and the surface roughness
(e.g., due to waves). The instrument was designed so that if the surface were liquid, the sounder would measure the speed of
sound in the "ocean" and possibly also the subsurface structure (depth). During descent, measurements of the speed of sound gave information on atmospheric composition and temperature, and an accelerometer recorded
the deceleration profile at impact, indicating the hardness and structure of the surface. A tilt sensor measured pendulum motion during the descent and was also designed to indicate the probe's attitude after landing and
show any motion due to waves. If the surface had been liquid, other sensors would also have measured its density, temperature and light reflecting properties, thermal conductivity, heat capacity, and electrical
properties (permittivity and conductivity). A penetrometer
instrument, that protruded 55mm past the bottom of the Huygens probe descent module, was used to create a penetrometer trace as
Huygens landed on the surface by measuring the force exerted on the instrument by the surface as the instrument broke though the
surface and was pushed down into the planet by the force of the probe landing itself. The trace shows this force as a function of
time over a period of about 400ms. The trace has an initial spike which suggests that the instrument hit one of the icy pebbles
on the surface photographed by the DISR camera.
The Huygens SSP was developed by Space Sciences Department of the University of
Kent and the Rutherford Appleton Laboratory Space Science Department under the direction of Professor John Zarnecki. The SSP research and responsibility transferred to the Open University when John Zarnecki transferred in 2000.
Spacecraft design
Application of
multi-layer insulation shimmers under bright lighting during final
assembly. The gold color of the MLI is due to light reflecting from the
aluminium coating on
the back of sheets of amber colored
Kapton.
Huygens was built under the Prime Contractorship of Aérospatiale in Cannes, France now part of Alcatel Alenia Space. The heat shield system
was built under the responsibility of Aérospatiale near Bordeaux, now part of EADS SPACE Transportation.
Parachute
Martin-Baker Space Systems was responsible for Huygens' parachute systems and the structural components, mechanisms and pyrotechnics that control the probe's descent
onto Titan. IRVIN-GQ was responsible for the definition of the structure of each of
Huygens' parachutes. Irvin worked on the probe's descent control sub-system under contract to Martin-Baker Space Systems.
A critical design flaw resolved
Long after launch, a few persistent engineers discovered that the communication equipment on Cassini had a potentially
fatal design flaw, which would have caused the loss of all data transmitted by the Huygens probe.
As Huygens was too small to transmit directly to Earth, it was designed to transmit the telemetry data obtained while
descending through Titan's atmosphere to Cassini by radio, which would in turn relay it to
Earth using its large 4-meter diameter main antenna. Some engineers, most notably ESA Darmstadt employees Claudio Sollazzo and Boris
Smeds, felt uneasy about the fact that, in their opinion, this feature had not been tested before launch under
sufficiently realistic conditions. Smeds managed, with some difficulty, to convince superiors to perform additional tests while
Cassini was in flight. In early 2000, he sent simulated telemetry data at varying power and
Doppler shift levels from Earth to Cassini. It turned out that Cassini was
unable to relay the data correctly.
The reason: under the original flight plan, when Huygens was to descend to Titan, it would have accelerated relative to
Cassini, causing its signal to be Doppler-shifted. Consequently, the hardware of
Cassini's receiver was designed to be able to receive over a range of shifted frequencies. However, the firmware failed to take into account that the Doppler shift would have changed not only the carrier frequency, but also the timing of the payload bits, coded by phase-shift keying at 8192 bits per second.
Reprogramming the firmware was impossible, and as a solution the trajectory had to be changed. Huygens detached a month
later than originally planned (December 2004 instead of November) and approached Titan in such a way that its transmissions
traveled perpendicular to its direction of motion relative to Cassini, greatly reducing the Doppler shift.[7]
The trajectory change overcame the design flaw for the most part, and data transmission succeeded, although the information
from one of the two radio channels was lost due to an unrelated error.
The trajectory change was not the only mitigation to the Doppler shift problem, and software patches were uplinked to several instruments on the
probe from the Deutsche Aerospace facility in Darmstadt to further reduce the risk of data loss.
"Channel A" data lost
Huygens was programmed to transmit telemetry and scientific data to the
Cassini orbiter for relay to Earth using two redundant S-band radio systems, referred to
as Channel A and B, or Chain A and B. Channel A was the sole path for an experiment to measure wind speeds by studying tiny
frequency changes caused by Huygens' motion. In one other deliberate departure from full redundancy, pictures from the
descent imager were split up, with each channel carrying 350 pictures.
As it turned out, Cassini never listened to channel A because of an operational commanding error. The receiver on the
orbiter was never commanded to turn on, according to officials with the European Space Agency. ESA announced that the program
error was a mistake on their part, the missing command was part of a software program developed by ESA for the Huygens
mission and that it was executed by Cassini as delivered.
The loss of Channel A means only 350 pictures were received instead of the 700 planned. Also all Doppler radio measurements between Cassini and Huygens were lost. Doppler radio
measurements of Huygens from Earth were made, though not as accurate as expected measurement that Cassini would
have made; when added to accelerometer sensors on Huygens and VLBI tracking of the position of the Huygens probe from Earth, reasonably accurate
wind speed and direction measurements can still be derived.
Amateur contributions
The Huygens mission benefited significantly from amateur contributions. This was enabled by the decision of the imaging
science Principal Investigator Marty Tomasko to make the image raw data of the DISR instrument available to the public. The many
small and low contrast images had to be assembled into mosaics and panoramas of the landing region in a time consuming process,
and space science enthusiasts all around the world began to deal with this challenge. Only some hours later the first mosaics of
the Huygens landing region were published,[8]
created by Daniel Crotty, Jakub Friedl, Ricardo Nunes and Anthony Liekens. Christian
Waldvogel published an improved and colorized Panorama. Another amateur, René Pascal, intensively engaged in the
Huygens image processing, developed a method to remove camera artifacts from the images and created a comprehensive mosaic
of the region now called Adiri.[9]
See also
References
- ^ Titan probe's pebble 'bash-down', BBC News, 10 April
2005.
- ^ New
Images from the Huygens Probe: Shorelines and Channels, But an Apparently Dry Surface, Emily Lakdawalla, 2005-01-15, verified 2005-03-28
- ^ M. Fulchignoni, F. Ferri, F. Angrilli, A.
Bar-Nun, M.A. Barucci, G. Bianchini, W. Borucki, M. Coradini, A. Coustenis, P. Falkner, E. Flamini, R. Grard, M. Hamelin, A.M.
Harri, G.W. Leppelmeier, J.J. Lopez-Moreno, J.A.M. McDonnell, C.P. McKay, F.H. Neubauer, A. Pedersen, G. Picardi, V. Pirronello,
R. Rodrigo, K. Schwingenschuh, A. Seiff, H. Svedhem, V. Vanzani and J. Zarnecki (2002). "The Characterisation of Titan's
Atmospheric Physical Properties by the Huygens Atmospheric Structure Instrument (Hasi)". Space Science Review 104:
395 - 431. DOI:10.1023/A:1023688607077.
- ^ Niemann HB, Atreya SK, Bauer SJ, Biemann K,
Block, Carigan GR, Donahue TM, Frost RL Gautier D, Habermann JA, Harpold D, Hunten DM, Israel G, Lunine JI, Mauersberger K, Owen
TC, Fraulin, Richards JE, Way, SH (2002). "The Gaschromatograph Mass Spectrometer for the Huygens Probe". Space Science
Review 104: 533-591. DOI:10.1023/A:1023680305259.
- ^ H. B. Niemann, S. K. Atreya, S. J. Bauer,
G. R. Carignan, J. E. Demick, R. L. Frost, D. Gautier, J. A. Haberman, D. N. Harpold, D. M. Hunten, G. Israel, J. I. Lunine, W.
T. Kasprzak, T. C. Owen, M. Paulkovich, F. Raulin, E. Raaen, S. H. Way (2005). "The abundances of constituents of Titan’s
atmosphere from the GCMS instrument on the Huygens probe". Nature
438: 77-9-784. DOI:10.1038/nature04122.
- ^ Israel G, Cabane M, Brun J-F, Niemann H,
Way S, Riedler W, Steller M, Raulin F, Cosica D (2002). "Huygens Probe Aerosol Collector Pyrolyser Experiment". Space Science
Review 104: 433-468. DOI:10.1023/A:1023640723915.
- ^ Oberg, James. "Titan
Calling", IEEE Spectrum, October 4, 2004.
(offline as of 2006-10-14, see Internet Archive version)
- ^ http://anthony.liekens.net/index.php/Main/Huygens
- ^ http://www.beugungsbild.de/huygens/huygens.html
External links
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