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Philae landing preview: What to expect on landing day

Posted by Emily Lakdawalla

05-11-2014 16:15 CST

Topics: Rosetta and Philae, mission status

The timeline is up-to-date as of November 12 at 07:30 UTC.

Ten years. That's how long it took Rosetta to get from Earth to comet 67P/Churyumov-Gerasimenko from its launch on March 2, 2004, to the beginning of its first orbit on August 6, 2014. For the Philae lander, bolted to the side of Rosetta, the journey has been slightly longer, and it's not quite over yet.

Philae has warmed up its science instruments and has even taken a couple of amazing photos of the comet with Rosetta's solar panel in the foreground, but the lander doesn't really begin to get to work until November 12 at 8:35 UT, when it will finally separate from the orbiter. Seven hours later, it will arrive at the surface of the comet. Hopefully, Philae will survive the landing, and begin to return data.

All next week, I'll be in Darmstadt, Germany, at the European Space Operations Centre (ESOC), to witness the historic attempt at landing on a comet. I'm not going to lie to you: I'm going to be terrified about Philae's survival until I see ESA engineers leaping from their seats and cheering. To be clear, I have no specific doubts about the spacecraft or its designers. It's just that we have never landed on anything like a comet before. We don't really know what the surface of a comet is like -- is it a hard, crusty shell of rocky material? A diaphanously fluffy, almost cloud-like layer of highly porous dust? Gravelly? Crunchy? Crystalline? Powdery? Sandpapery? Slippery? Who knows? The last time we landed on a surface that we knew so little about was when ESA landed Huygens on Titan in 2004. But Huygens did almost all of its science on the way down, returning all its data to the Cassini orbiter in real time, so it didn't matter whether Huygens survived its arrival on Titan's surface. In contrast, almost all of Philae's science will not come until after a successful landing. It's going to be terrifying. But I wouldn't miss it for the world.

What will we know, when? Below is a timeline of Philae events, and a brief summary of what Philae intends to do. Media-related events are highlighted yellow; mission control events in orange; and the major separation and landing events in red, most of it taken from this timeline released November 7 by ESA (PDF).

 Time at spacecraftTime on Earth
Rosetta Google Hangout -- -- Nov 7 16:00 Nov 7 15:00 Nov 7 07:00
ESOC media update (ESA TV) -- -- Nov 10 15:00 Nov 10 14:00 Nov 10 06:00
ESOC media update (ESA TV) -- -- Nov 11 11:00 Nov 11 10:00 Nov 11 02:00
Lander switch-on -14h 30m Nov 11 18:05 19:33 18:33 10:33
Lander batteries and compartment heating; ADS tank opening -13h 58m 18:37 20:05 19:05 11:05
Lander primary battery condition start -13h 38m 18:57 20:25 19:25 11:25
24-hour ESA #CometLanding Livestream begins -- -- 20:00 19:00 11:00
ESOC media update (ESA TV) -- -- 20:00 19:00 11:00
Go/no-go decision 1: ESOC Flight Dynamics confirms Rosetta on correct trajectory -- -- 20:30 19:30 11:30
Rosetta starts slew to pre-delivery attitude (expected loss of signal) -13h 19:34 21:03 20:03 12:03
End of Rosetta slew -12h 20m 20:14 21:43 20:43 12:43
Start lander flywheel operation -12h 11m 20:24 21:52 20:52 12:52
Go/no-go decision 2: Confirm lander sequence and Rosetta ready for separation -- -- Nov 12 01:00 Nov 12 00:00 16:00
Lander generates final telemetry for separation decision -8h Nov 12 00:35 02:03 01:03 17:03
Go/no-go decision 3: Confirm Philae ready for landing (This decision was delayed about an hour due to problem with cold-gas jet system on lander) -- -- 03:35 02:35 18:35
Start switching lander instruments on; ROMAP is first -5h 03:35 05:03 04:03 20:03
Rosetta start executing on-board commands for delivery operations -4h 35m 04:00 05:28 04:28 20:28
Start heating lander batteries to separation temperature -4h 29m 04:06 05:34 04:34 20:34
Rosetta pre-delivery maneuver (lining up for separation) -2h 33m 06:01 07:30 06:30 22:30
Go/no-go decision 4: proceed for landing -- -- 08:05 07:05 23:05
Switch on MUPUS -1h 14m 07:21 08:49 07:49 23:49
Start MUPUS operation; switch on CIVA and ROLIS imagers -1h 11m 07:24 08:52 07:52 23:52
Start CIVA and ROLIS; switch on SESAME dust sensor -1h 8m 07:27 08:55 07:55 23:55
Start SESAME 0h 59m 07:36 09:04 08:04 Nov 12 00:04
Turn on separation mechanical systems 0h 17m 08:18 09:46 08:46 00:46
Start CONSERT on orbiter 0h 14m 08:21 09:49 08:49 00:49
Start CONSERT on lander 0h 13m 08:22 09:50 08:50 00:50
Start internal automated sequence to prepare for landing 0h 11m 08:23 09:51 08:51 00:51
Lander to internal battery power 0h 10m 08:25 09:53 08:53 00:53
 Time at spacecraftTime on Earth
Lander separation, 94-second window, separation at 18 cm/s, 22.5 km from comet. Separation, Descent, and Landing phase begins +0h 08:35 10:03 09:03 01:03
Lander CIVA camera photographs orbiter (FAREWELL1) +0h 08:35 10:04 09:04 01:04
Lander CIVA camera photographs orbiter (FAREWELL2) +0h 2m 08:37 10:06 09:06 01:06
Lander/orbiter separation distance 100m; earliest landing gear and ROMAP boom deployment +0h 8m 08:43 10:12 09:12 01:12
Lander begins rotation of 14 degrees to stable landing orientation +0h 22m 08:57 10:25 09:25 01:25
Rosetta divert maneuver; loss of signal due to slew +0h 40m 09:15 10:43 09:43 01:43
Lander completes post-separation activities +0h 43m 09:18 10:47 09:47 01:47
Acquisition of signal from lander +1h 50m 10:25 11:53 10:53 02:53
Start of downlink of stored data, including CIVA "farewell" image +2h 55m 11:31 13:00 12:00 04:00
Earliest possible release of NavCam and/or CIVA "farewell" images -- -- 13:40 12:40 04:40
NASA TV coverage begins -- -- 15:00 14:00 06:00
Start CIVA and ROLIS; switch on lander anchor +5h 55m 14:30 15:58 14:58 06:58
Start imaging landing site; switch on active descent system (cold jets that will push lander against surface) +5h 58m 14:33 16:01 15:01 07:01
ROLIS begins imaging +6h 3m 14:38 16:07 15:07 07:07
Lander completes pre-touchdown operations +6h 13m 14:48 16:17 15:17 07:17
Start of lander touchdown window +6h 18m 14:54 16:22 15:22 07:22
 Time at spacecraftTime on Earth
Expected Landing (time approx). Thruster fires for 15 seconds; harpoons fire; flywheel turns off. Note: times for subsequent events are relative to actual landing time. +7h 15:35 17:03 16:03 08:03
CIVA panoramic imaging (transmitted to Rosetta immediately) Landing +0h 3m 15:38 17:07 16:07 08:07
Ptolemy and COSAC begin science; descent data transmitted to Rosetta Landing +0h 3m 15:38 17:07 16:07 08:07
NASA TV coverage ends -- -- 17:30 16:30 08:30
Lander completes separation, descent, and landing phase, uploads data Landing +0h 36m 16:11 17:39 16:39 08:39
Earliest possible presentation of first images -- -- 18:00 17:00 09:00
First science sequence begins Landing +1h 45m 17:20 18:49 17:49 09:49
24-hour ESA #CometLanding Livestream ends -- -- 19:00 18:00 10:00
End of first lander/orbiter communication window Landing +2h 59m 18:34 20:03 19:03 11:03
ESOC media update (ESA TV) -- -- Nov 13 14:00 Nov 13 13:00 Nov 13 05:00
First science sequence ends Landing +65h Nov 15 08:35 Nov 15 10:03 Nov 15 09:03 Nov 15 01:03

A note on timing. Events are shown in both spacecraft event time (SCET) -- the time on the spacecraft's clock, which will correspond to timestamps on images and data -- and in Earth time (Universal, Central European, and Pacific time zones). On the day of landing, the comet will be about 510 million kilometers from Earth, so one-way light time between the spacecraft and Earth is just shy of half an hour (28 minutes 20 seconds, to be exact). For events that will take place aboard spacecraft, like rocket maneuvers, I take spacecraft time from the ESA published timeline and add one-way light time to get Earth time, because that is the time on Earth that we should hear that those events happen. The first version of this timeline is almost certain to contain some errors; I will update this post to correct those and add more information as I find it. The graphical timeline below, which came from ESA, is actually a mix of spacecraft and Earth event times, confusingly. Other sources of timeline information include the ESA TV website and the ESA invitation to media.

Graphical timeline of the Philae landing


Graphical timeline of the Philae landing
Rosetta moves from lower right to upper left in this diagram. T0 -- the time of separation -- is November 12 at 08:35 UT, according to the spacecraft's clock. "GONOGO" points along the timeline indicate places where the spacecraft waits for permission to proceed from Earth before performing irreversible actions like separating the lander. With a half-hour one-way light time between Rosetta and Earth, it takes at least an hour for Rosetta to send telemetry to Earth and then receive an instruction in response to that telemetry.

Philae's instruments: A brief guide

Science instruments come in two types: remote sensing (which detect things from a distance) and in-situ (which must be in contact with what they measure). Philae can use its remote sensing instruments during descent, but the in-situ instruments don't get to operate until after landing.

  • Remote sensing instruments include the CIVA and ROLIS imagers and CONSERT radar sounder. CIVA's 6 cameras can produce panoramic images of the comet's surface; the side-looking ones have produced Rosetta's iconic self-portraits. ROLIS is intended to provide context images for in-situ measurements; it will take photos during descent. CONSERT has components on both orbiter and lander; it transmits radio waves from orbiter to the lander, sometimes through the comet itself.
  • Because magnetic fields and plasma exist in the space around a comet, not just on the surface, one in-situ instrument will be able to operate during descent: the Rosetta Lander Magnetometer and Plasma Monitor (ROMAP). ROMAP studies the magnetic field and interaction between comet and solar wind.
  • In-situ instruments include the Alpha Particle X-Ray Spectrometer (APXS), the Cometary Sampling and Composition Experiment (COSAC), Multi-Purpose Sensors for Surface and Subsurface Science (MUPUS), Ptolemy, and the Surface Electrical Sounding and Acoustic Monitoring Experiments (SESAME), which will only be used after landing. APXS measures elemental composition. COSAC and Ptolemy are evolved-gas analyzers, which can determine molecular and isotopic composition from samples delivered to it by Philae's drill and sampling mechanism (SD2). MUPUS and SESAME are suites of sensors that will measure the physical properties of the comet's surface.
Philae's instruments

ESA / ATG medialab

Philae's instruments
Philae has 10 instruments:
APXS: Alpha Particle X-ray Spectrometer, for studying elemental composition
CIVA: Comet Nucleus Infrared and Visible Analyser, six black-and-white cameras for panoramic imaging
CONSERT: COmet Nucleus Sounding Experiment by Radiowave Transmission, for studying comet interior
COSAC: The COmetary SAmpling and Composition, an evolved gas analyzer for identifying organic molecules
Ptolemy: an evolved gas analyzer for measuring isotopes of light elements
MUPUS: MUlti-PUrpose Sensors for Surface and Sub-Surface Science, for studying comet physical properties
ROLIS: Rosetta Lander Imaging System, will provide context images of landing site
ROMAP: Rosetta Lander Magnetometer and Plasma Monitor, for studying the magnetic field and plasma environment of the comet
SD2: Sampling, drilling and distribution subsystem, can drill to 23 centimeters depth
SESAME: Surface Electric Sounding and Acoustic Monitoring Experiment, for studying comet physical properties

Setting Up for Landing

Philae will land at a site named "Agilkia" for an island in the Nile river in a public contest. Agilkia is on the smaller of the comet's two lobes, though not on the end; hopefully CONSERT will be able to see completely through the small lobe when Rosetta is in the right position.

Philae's selected landing site:

ESA / Rosetta / NavCam / MPS for OSIRIS Team MPS / UPD / LAM / IAA / SSO / INTA / UPM / DASP / IDA

Philae's selected landing site: "Agilkia"
Rosetta NavCam and OSIRIS views of the selected primary landing site for Philae. The Navcam image of the whole comet was taken on August 16, 2014 from a distance of 100 kilometers; the comet is about 4 kilometers across. The OSIRIS image was taken on August 20, 2014 from a distance of 67 kilometers. The "+" marks the center of the landing site; the square is about 1 kilometer on a side. The site was named "Agilkia" in a public contest.

To deliver Philae to Agilkia, Rosetta fires rockets to put it on a collision course with the comet. Back on Earth, mission controllers will check that the maneuver was successful and on target before delivering the "go for separation" command. With a half-hour one-way light time between Rosetta and Earth, this cycle will take an hour to complete. Two hours after the pre-delivery maneuver, Rosetta will release Philae. Forty minutes after that, Rosetta will perform a divert maneuver, allowing it to continue onward to a relay orbit around the comet, from which Rosetta can receive Philae transmissions and perform the CONSERT experiment.

Here is a Youtube video that shows the crazy maneuvering of Rosetta for landing and relay operations in great detail. I've pulled out the frames right around the landing so that you can see how the motion of Rosetta and rotation of the comet fit together to deliver Philae to the landing site.

Delivering Philae to Agilkia


Delivering Philae to Agilkia
On November 12 at about 6:35 UT, Rosetta will place itself on a collision course with comet Churyumov-Gerasimenko. Two hours later, the Philae lander will separate. Another 40 minutes after that, the orbiter will perform a divert maneuver to put it into a relay orbit. Landing is expected to happen at about 15:35 UT, with confirmation received on Earth about 30 minutes later. (Clip from this longer YouTube video)

Separation, Descent, and Landing

Separation, Descent, and Landing (SDL) events are described in detail on the Rosetta blog.


The lander will be pushed from the orbiter at a commanded, precise speed. If the commanded deploy does not succeed, a backup spring can push the lander off at a speed of 18 centimeters per second. CIVA will take a "farewell" image of the orbiter, which should be returned during the descent. Hopefully Rosetta's NavCam will capture the return image, of Philae departing.


It will take Philae 7 hours to free-fall the 22.5 kilometers to Churyumov-Gerasimenko's surface. Within an hour of separation, Philae will establish radio contact with Rosetta, unfold its three-legged landing gear, deploy the CONSERT radio antenna, deploy the boom holding the ROLIS camera, and begin taking photos with ROLIS.

Forty minutes after separation, Rosetta will perform a divert maneuver. Two hours after separation, Rosetta will turn to watch Philae drift toward the comet.

Throughout its descent, Philae will be actively gathering data. ROLIS will shoot descent images. COSAC, Ptolemy, and SESAME will attempt to sample gas and dust around the comet. ROMAP and SESAME will measure magnetic fields and plasma. CONSERT will measure the separation between lander and orbiter, and also try to actively sense the surface of the comet.

A little of the descent data will be transmitted to Rosetta during the descent, so regardless of what happens to Philae when it contacts the comet, there will be some science returned. Descent data may include the CIVA farewell image and CONSERT data on the range from orbiter to lander with respect to time, among other information. (Ref)


Philae's legs are designed to damp out the forces of a hard landing to reduce the lander's chance of bouncing. When Philae touches down, it will fire two harpoons to attach it firmly to the comet's surface. A thruster on top of the lander fires at the same time as the harpoons, keeping the lander on the ground. Ice screws also deploy from the three lander feet.

Upon landing, the first science activities will be CIVA panoramic imaging, MUPUS acceleration measurements, and SESAME elastic properties measurements. The descent data and these first images will be returned as soon as possible so that mission engineers can determine the orientation of the lander, and then command it to rotate it to best illuminate its solar panels and optimize the positions of the lander instruments. Mission engineers will also use these early data to calculate tables describing when the orbiter will be visible from the lander (for communication) and when the ground will be illuminated. (Ref)

If the comet turns out to be very soft (with a compressive strength less than 2 kPa, similar to lightly compacted snow), the lander could sink in up to its baseplate, which would prevent it from rotating. The lander would only sink farther if the compressive strength were less than 100 Pa (similar to powder snow). (Ref 1, ref 2)

The first science sequence lasts five days and can be performed entirely under battery power; with solar power, the lander could survive and continue doing science for much longer. For more post-landing plans, read the Rosetta blog.

Whatever happens on landing day, I'll be there to report it! Stay tuned to this blog, to my Twitter feed, and to my list of official Rosetta and Philae tweeters for news.

ESA / ATG medialab

Video: Philae touchdown!
Visualisation of the deployment of the Philae lander from Rosetta at comet 67P/Churyumov-Gerasimenko in November 2014. Rosetta will come to within 2.5 km of the comet’s surface to deploy Philae, which will then take around 2 hours to reach the surface.
See other posts from November 2014


Or read more blog entries about: Rosetta and Philae, mission status


ethanol : 11/05/2014 05:56 CST

Does anyone know if Philae has reaction wheels for controlling its orientation? And if so, how is orientation measured? Does it use the CIVA cameras as star finders, or somehow orient to Rosetta's signal? I know they must have addressed this somehow, but I have this terrible image of Philae very slowly tumbling after ejection, and landing wrong-side-up.

Weywot: 11/06/2014 03:37 CST

Philae has one reaction wheel for the z-axis to maintain the upright position. It is spun up prior to separation and consumes 6W. A complete set of three wheels was deemed too costly, too heavy and would have consumed too much energy

ethanol: 11/06/2014 11:05 CST

Thanks Weywot, That makes sense: as long as you release with the right orientation all you need is a gyroscope.

quetzalcoatl: 11/06/2014 12:08 CST

Hello everybody! The new name for site J is Agilkia.

lodaya: 11/07/2014 12:02 CST

From the video it appears that the "firing distance" is about 15 km and the area of the comet head available for landing after calculation of the rotation is about 2 km: that is, if the direction is off by about 8 degrees the lander will not only miss Agilkia it will miss the comet altogether. A darts player will not find that too bad. Hitting the bull's eye (Agilkia) is of course harder for non-expert throwers. The really difficult part is imagining how many different angles and feature possibilities there are when approaching (think of an irregular dartboard but having to land the dart perpendicular to the surface), and having programmed the lander to handle all of them.

Haerwe: 11/07/2014 05:34 CST

ESA has decided to delay the release of the OSIRIS results for 6 month. The reason is to protect the advantage of being first to publicise new scientific findings Well there is a certain rationale supporting such a policy I admit. I personally support a different handling - anyway. The question now is how will ESA handle the Philae images. Since the image resolution is expected to be way higher than OSIRIS will we have to expect the Philae images SIX MONTH LATER ? That implies we will see Philae images in May or June 2015 if at all Remember - the Principal Investigator/OSIRIS prior to Mr. Sierks (Dr. Uwe Keller) withheld OSIRIS Images taken during the Mars flyby 2007 for at least FIVE YEARS

Michael Richmond: 11/07/2014 12:47 CST

Emily wrote: > It's just that we have never landed on anything like a comet before. We don't really know what the surface of a comet is like -- is it a hard, crusty shell of rocky material? A diaphanously fluffy, almost cloud-like layer of highly porous dust? Gravelly? Crunchy? Crystalline? Powdery? Sandpapery? Slippery? Who knows? The last time we landed on a surface that we knew so little about was when ESA landed Huygens on Titan in 2004. Are you forgetting when Hayabusa landed on asteroid Itokawa in 2005? The surface gravity of Itokawa was similar to that of 67P/Churyumov-Gerasimenko. Sure, one is an asteroid and one is a comet, but there are a number of asteroids which turned out to be defunct comets, so the difference in surface properties may be very small.

ethanol: 11/07/2014 05:48 CST

Michael, From what I can find, Hayabusa was not equipped to measure material properties of itokowa's surface (and in any case it was designed not so much to "land" but contact briefly with a sampling horn). Additionally, rosetta is an active comet, and we might expect its surface to be composed of material recently deposited from its jets, and probably very different chemical composition than the rocky material sampled from itokowa. So no, we really don't know what the surface will be like.

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