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The Landing of Rosetta's Philae Lander on Comet 67P/Churyumov-Gerasimenko

thumbnail to larger farewell images views in the form of a animated gif of the lander seen separating from the Rosetta orbiter click to larger farewell images views in the form of a animated gif of the lander seen separating from the Rosetta orbiter. picture ESA

As the landing date was to be confirmed on 26 September after further trajectory analysis and the final Go/No Go for a landing at the primary site following a comprehensive readiness review on 14 October, the landing operations began since Nov. 11, 2014. After a series of Go/No go decisions were made, the Rosetta probe was eventually moved to a point about 14 miles above the comet's surface, and separation was confirmed at ESA’s Space Operation Centre, ESOC, in Darmstadt, Germany at 09:03 GMT as it took the radio signals from Rosetta 28 minutes and 20 seconds to reach Earth. Thence, Philae kept descending without propulsion or guidance, gradually gathering speed in the comet's weak gravitational field during about 7 hours, and eventually reaching a speed of 3 ft per second only. Commands prepared by the German space agency DLR's Lander Control Center had been uploaded via the Rosetta mission control before separation. During the descent, the lander was to take pictures and make science, and it was to begin communications with Rosetta about two hours after separation. All that occurred by 311 million miles from the Earth. By November 2014, the 'Site J' landing site had been renamed for Agilkia Island, a island on the Nile River in the south of Egypt where the Temple of Isis from the island of Philae when the latter was flooded during the building of the Aswan dams

Some troubles hampered the landing of the Philea lander however. First, the cold gas thruster atop of the lander did not appear to be working so the landing had to rely on the lander's harpoons only at touchdown. Those harpoons in turn were not available at landing, which made that the lander bounced off the landing site by 1 kilometer (300 ft), despite touchdown occurred at a walking pace (which is due to the comet's weak gravity with the lander weighing 1 gram only instead of 50 lbs!), and it eventually landed on a inclined terrain, close to a boulder, and in shadow. The lander after landing thus is just anchored with the comet through two of its three ice screws only. With a inclination of 13° and 1 hour and 30 mn of solar light available instead of 12, the lander is hampered in his science but that kept up however. Philae’s Science, Operations and Navigation Centre is at France's CNES space agency, and the Lander Control Centre at DLR, the German space agency

thumbnail to a view of the comet's surface closing as seen by the Philae lander's ROLIS instrument click to a view of the comet's surface closing as seen by the Philae lander's ROLIS instrument. picture ESA
thumbnail to a two-image mosaic of the neighbourhood of where the lander touchdowned. One of the lander’s three feet can be seen in the foreground click to a two-image mosaic of the neighbourhood of where the lander touchdowned. One of the lander’s three feet can be seen in the foreground. picture ESA

Confirmation of Philae’s touchdown on the surface of comet 67P/Churyumov–Gerasimenko had arrived on Earth at 16:03 GMT on Nov. 12, 2014. A first touchdown and its signal however occurred as the lander bounced off downrange the planned landing ellipse. Philae touched down again then two hours after as third contact was the charm. The lander however alighted in a crevice about six feet (two meters) in diameter and six feet (two meters) deep and it lied on its side. Despite is landing site position, the Philae lander has completed its planned primary science mission, of which a drill into the soil, after nearly 57 hours on comet 67P/Churyumov–Gerasimenko, performing on its own batteries. The Philae probe has detected organic molecules in the atmosphere of comet 67P/Churyumov-Gerasimenko. The lander’s body was lifted by about 4 cm (less than 2 inches) and rotated about 35° in an attempt to receive more solar energy but Philae’s power rapidly depleted. Descent images show that the surface of the comet is covered by dust and debris ranging from a line in size to 3 feet while post-landing panoramic images show layered walls of harder-looking material. As the illumination at the site is unsufficient to provide more power, the Philae team decided to put the lander into hibernation as they hope they might be able to wake it up when closer to the Sun with enough solar power. The Rosetta orbiter will listen for a signal each time its orbit brings it into line-of-sight visibility with the lander as it is unlikely that contact will be re-established with the lander in the near future. The lander could be woken up on 26 April 2015, but had been unable to send any signals until 13 June. After 13 June, it made a further seven intermittent contacts with Rosetta in the following weeks, with the last coming on 9 July. That awakening is due to that the comet came closer to Sun on its orbits, yielding more power to the landing's solar panels. However, such communications links were too short and unstable to enable any scientific measurements to be commanded. The Philae lander however had managed to complete 80 percent of its planned first science sequence before falling into hibernation. Philae's mission was considered decommissioned by ESA by late Dec. 2015

ESA's Philae Landing Operations Timeline

(this timeline is a one given by ESA; all times subject to change. check abbreviations below)

Date UTC
on Earth
CET
on Earth
Event
11/11 01:48:49 02:48:49 BOT ESA New Norcia (NNO)
11/11 03:10:00 04:10:00 BOT NASA DSN Canberra
11/11 12:25:00 13:25:00 EOT Canberra
11/11 13:40:00 14:40:00 BOT DSN Madrid
11/11 13:58:05 14:58:05 BOT ESA Malargüe (MLG)
11/11 14:00:00 15:00:00 Flight Dynamics Team at ESOC begin orbit determination procedure to accurately fix Rosetta's precise trajectory
11/11 14:30:17 15:30:17 EOT ESA NNO
11/11 18:33:20 19:33:20 Lander switch-on. Includes switching on Electrical Support System, which controls orbiter communication interface with the lander
11/11 19:05:20 20:05:20 Lander batteries and compartment heating
ADS Tank (Active Descent System - provides cold gas thrust upwards to avoid rebound upon landing) opening
11/11 19:25:20 20:25:20 Lander Primary Battery conditioning start; about 28 mins
11/11 19:00:00 20:00:00 EOT DSN Madrid
11/11 19:30:00 20:30:00 GO/NOGO1 - Last full orbit determination; ESOC Flight Dynamics confirms Rosetta trajectory is correct
11/11 20:03:00 21:03:00 Rosetta starts slew to pre-delivery manoeuvre attitude (expected loss of signal)
11/11 20:20:00 21:20:00 BOT DSN Goldstone
11/11 20:43:00 21:43:00 End of Rosetta slew
11/11 20:52:20 21:52:20 Start Lander flywheel operation - provides stability during descent
11/11 23:25:00 00:25:00 BOT DSN Goldstone
11/11 23:40:00 00:40:00 BOT DSN Canberra
12/11 00:00:00 01:00:00 EOT DSN Goldstone
12/11 00:00:00 01:00:00 GO/NOGO 2(a) - Confirm telecommands to control delivery sequence are ready
GO/NOGO 2(b) - ESOC confirms Rosetta is ready
12/11 01:00:00 02:00:00 ESOC uploads commands to control spacecraft for Lander delivery operations
12/11 01:03:20 02:03:20 Lander generates final telemetry (TM) on-board prior to GO/NOGO for SEP decision
12/11 01:35:00 02:35:00 (EXPECTED AT 02:35 UTC / 03:35 CET) GO/NOGO 3 - Confirm Philae is ready for landing
12/11 01:46:10 02:46:10 BOT ESA New Norcia
12/11 03:02:50 04:02:50 EOT ESA Malargüe
12/11 04:03:20 05:03:20 Lander - start of Separation, Descent & Landing (SDL) activities
Start switching Lander instruments ON; ROMAP first
12/11 04:28:20 05:28:20 Rosetta - Start executing on-board commands for delivery operations
12/11 04:34:20 05:34:20 Start heating Lander batteries to separation temperature
12/11 06:03:20 07:03:20 Rosetta - Earliest start pre-delivery manoeuvre (thruster burn)
Burn will be followed by loss of signal due to subsequent slew for separation
Manoeuvre expected to be about 0.46m/s & about 6 mins duration
Date UTC
on Earth
CET
on Earth
Event
12/11 06:35:00 07:35:00 Earliest GO/NOGO 4 - final decision to go for landing
12/11 07:03:20 08:03:20 Rosetta - Latest start pre-delivery manoeuvre
12/11 07:35:00 08:35:00 Latest GO/NOGO 4 - final decision to go for landing
- - Following MVR, ESOC Flight Dynamics Team conducts rapid assessment of MVR performance to verify burn results
12/11 07:49:20 08:49:20 Lander - Switch on MUPUS
12/11 07:52:20 08:52:20 Start MUPUS operation and switch-on CivaRolis
ÇIVA and ROLIS are imaging systems; ÇIVA makes panoramic images, ROLIS looks down
12/11 07:55:20 08:55:20 Start CivaRolis operation and switch-on SESAME (dust sensor)
12/11 08:04:20 09:04:20 Start SESAME operation
12/11 08:46:20 09:46:20 Start MSS (Mechanical Support System), which executes the mechanical separation from the Orbiter
12/11 08:46:20 09:46:20 Separation Motors ON
12/11 08:49:20 09:49:20 Start CONSERT Orbiter operation
12/11 08:50:20 09:50:20 Start CONSERT Lander operation
12/11 08:51:20 09:51:20 Start MSS sequence - internal autosequence to prepare for landing
12/11 08:53:20 09:53:20 Lander now on internal battery power
12/11 - - Screws in Separation Motors start to rotate and impart deployment speed to push Lander away, retrograde .21 m/s
12/11 09:03:20 10:03:20 PHILAE SEPARATION (Forecast; 94-sec window)
Separation confirmation received on ground via ESA's NNO New Norcia station
12/11 09:04:12 10:04:12 Lander (ÇIVA) obtains first images of Orbiter (FAREWELL1)
12/11 09:06:17 10:06:17 Lander (ÇIVA) obtains seconds images of Orbiter (FAREWELL2)
12/11 09:12:17 10:12:17 Lander / Orbiter separation distance now ~100m
Earliest autodeployment of landing gear and ROMAP boom antenna
12/11 09:25:50 10:25:50 Lander starts rotation of 14 degrees to stable landing orientation
12/11 09:43:20 10:43:20 Rosetta performs post-delivery manoeuvre
Burn will be followed by loss of signal due to subsequent slew back to nominal pointing
Manoeuvre magnitude to be determined on 12/11
12/11 09:47:17 10:47:17 Lander completes all post-separation activities
12/11 10:53:20 11:53:20 Acquisition of signal (AOS) from Rosetta
Expected AOS; link with Rosetta now re-established
12/11 11:59:20 12:59:20 Start of stored data downlink from Rosetta & Philae
12/11 12:20:00 13:20:00 EOT DSN Canberra
12/11 13:15:00 14:15:00 BOT DSN Madrid
12/11 13:55:00 14:55:00 BOT ESA MLG
12/11 14:27:00 15:27:00 EOT NNO
12/11 14:58:57 15:58:57 Lander - switch-on Anchor & CivaRolis
Date UTC
on Earth
CET
on Earth
Event
12/11 15:01:57 16:01:57 Lander - start imaging landing site and switch on ADS (Active Descent System)
12/11 15:07:02 16:07:02 ROLIS begins imaging
12/11 15:17:15 16:17:15 On board Lander, systems conduct final pre-touch-down operations
12/11 15:22:20 16:22:20 Start of Lander touch-down window
12/11 16:02:20 17:02:20 EXPECTED LANDING and receipt of signal (Forecast; 40 min variability)
12/11 - - Upon landing - start post-touch-down operations including:
* ADS thruster fires for ~15 sec to avoid rebound
* Harpoons (X2) fire to secure Lander to surface
* Flywheel off
12/11 16:07:12 17:07:12 ÇIVA-P panoramic imaging on
Lander obtains first images of surface and transmits same (forecast; depends on landing time)
12/11 16:07:14 17:07:14 Separation, Descent & Landing (SDL) science observations continue: Ptolemy & COSAC begin science gathering; data collected during descent and initial surface observations will be uploaded
12/11 16:39:39 17:39:39 Lander completes SDL operations; upload of science data
12/11 17:49:07 18:49:07 Lander begins First Science Sequence (FSS) Block 1; runs about 7 hours
12/11 19:00:00 20:00:00 EOT DSN Madrid
12/11 19:03:00 20:03:00 End of Lander/Orbiter first communication window
13/11 01:43:00 02:43:00 BOT ESA NNO
13/11 02:59:00 03:59:00 EOT ESA MLG

back Abbreviations

BOT Begin of track
EOT End of track
NNO ESA - ESTRACK 35m New Norcia tracking station, Australia
MLG ESA - ESTRACK 35m Malargüe tracking station, Argentina
LDR Philae Lander
ROS Rosetta Orbiter
LCC Lander Control Centre, DLR/Cologne
ESOC Rosetta Control Centre, ESA/Darmstadt
ROLIS Rosetta Lander Imaging System (ROLIS): CCD imager designed to return images of the landing site before and after Philae has landed
ADS Active Descent System (ADS) - this system emits cold gas thrust at touchdown to avoid rebound.
BOT Indicates when station is pointing & ready. Actual acquisition of signal may come only afterwards
DSS 25 NASA - DSN 34m Goldstone tracking station, California, USA
DSS 45 NASA - DSN 34m Canberra tracking station, Australia
DSS 55 NASA - DSN 34m Madrid tracking station, Spain
DSS 54 NASA - DSN 34m Madrid tracking station, Spain
MVR Manoeuvre - a thruster burn to change direction and/or speed
MSS (Mechanical Support System) is the lander side of Philae which executes the mechanical separation from the orbiter.
ESS ESS (Electrical Support System) is the orbiter part of the lander. The ESS controls the orbiter communication interface with the lander. ESS itself operates as usual as power and data interface to the Orbiter.
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