Cassini Significant Events for 09/07/06 - 09/13/06
The most recent spacecraft telemetry was acquired Wednesday, September 13, from the Goldstone tracking stations. The Cassini spacecraft is in an excellent state of health and is operating normally. Information on the present position and speed of the Cassini spacecraft may be found on the “Present Position” web page located at http://saturn.jpl.nasa.gov/operations/present-position.cfm .
Thursday, September 7 (DOY 250):
The Titan 17 flyby (T17), at 1000 km altitude, occurred September 7, 2006. This flyby was at a latitude of 23 degrees, in a region where the Titan atmospheric model predicted the atmospheric density to be greater than at higher latitudes. The project anticipated thruster duty cycling between 40 and 65%, and developed an on-the-shelf reference trajectory to increase the altitude of the T20 flyby should it be necessary. The duty cycle calculated by AACS after the flyby was considerably lower than expected, around 20%.
Prior to closest approach, the Imaging Science Subsystem (ISS) searched for and monitored lightning and aurora, and the Visible and Infrared Mapping Spectrometer (VIMS) worked on Titan mapping, monitoring, and photometry, and observed a stellar occultation through Titan’s atmosphere.
Titan closest approach was designed with a spacecraft attitude suitable for both Ion and Neutral Mass Spectrometer (INMS) data acquisition and a short Synthetic Aperture RADAR (SAR) swath of Titan’s surface. INMS data will be used to help determine atmospheric and ionospheric thermal structure. The Optical Remote Sensing (ORS) instruments used the time just after closest approach to continue Titan global mapping and atmospheric analysis.
The Cassini Plasma Spectrometer (CAPS), Cosmic Dust Analyzer (CDA), Ion and Neutral Mass Spectrometer (INMS), Magnetometer Subsystem (MAG), Magnetospheric Imaging Instrument (MIMI), and Radio and Plasma Wave Science (RPWS) instrument performed under the Magnetospheric and Plasma Science campaign to make inbound approach observations, provide context for the interaction between Titan and Saturn’s magnetosphere, and determine atmospheric and ionospheric thermal structures.
Friday, September 8 (DOY 251):
The S23 Saturn solar occultation Live Movable Block (LMB) kickoff meeting was held today. A typical schedule for an LMB process runs from five to seven days and looks something like this:
LMB kickoff meeting Friday (DOY 251)
Orbit Determination file available Saturday (DOY 252) at 2300 PDT
Epoch update and science analysis Sunday (DOY 253)
Go-No/Go meeting Monday (DOY 254)
Command Approval Meeting Tuesday (DOY 255) at 1600 PDT
Uplink Wednesday (DOY 256) Execution beginning on Friday (DOY 258)
The S23 leads uplinked files for an Enceladus Live Inertial Vector Propagator Update to execute tomorrow, September 9, and a RADAR Enceladus trigger. Both files have been verified onboard and should execute as planned.
Today concluded the T17 encounter activities. The Imaging Science Subsystem (ISS) used the Narrow Angle Camera to monitor surface and atmosphere changes and attempt to see surface color variations on Titan. The spacecraft performed a 9-hour downlink to the Goldstone 70-meter DSN antenna to play back the Titan flyby data.
After playback, the spacecraft turned its attention to Saturn’s rings and Iapetus. The ISS instrument made a series of zero-phase Iapetus observations and captured five Optical Navigation images. CIRS gathered temperature data on the rings, while UVIS used the opportunity for spectral mapping of the rings.
Saturday, September 9 (DOY 252):
Non-targeted flybys of Atlas, Methone, Calypso, and Enceladus occurred today. The Enceladus flyby was at an altitude of 39,932 km.
The first Cassini Radio Science Subsystem (RSS) Saturn gravity observation in Orbit 28 concluded successfully today. The observation consisted of one segment slightly over 6 hours in duration, and almost centered on periapsis. This was the first of two RSS Saturn gravity observations during the Cassini Tour that were selected as a pair. These two observations are specifically optimized for measurement of the gravity field of Saturn. The second occurs during Orbit 68 in May of 2008.
Sunday, September 10 (DOY 253):
Orbit trim maneuver #71 was performed today. This was the T17 post flyby cleanup maneuver. The main engine burn began at 12:23 PM. Telemetry immediately after the maneuver showed a burn duration of 41.0 seconds, giving a delta-V of 6.55 m/s. All subsystems reported nominal performance after the maneuver. The next maneuver, OTM-072, is scheduled for Thursday, September 14.
Monday, September 11 (DOY 254):
It turns out that S25 is in conflict with the Messenger Project on October 24, DOY 297, for Deep Space Station 14. Messenger has a critical event, the Venus-1 flyby, on that day. DSS-14 is required by Messenger to downlink the flyby data. The current proposal is for Cassini to keep the first 3 hours over DSS-14 and then hand over to DSS-15 for the remaining 6 hours of the pass. Messenger will then have the remaining 6 hours over DSS-14 for downlink.
The Titan Atmosphere Model Working Group (TAMWG) met today to review the T17 Titan flyby results and to recommend whether the T20 closest approach altitude should be raised. T17 is significant because it is, at closest approach, the lowest latitude flown to date at 23=B0. The results from AACS, INMS, and Navigation showed the atmospheric density significantly lower than predicted. As a result, the previous model, which assumed an increase in density near the equator, is under serious question.The flybys for T18 on September 23 and T19 on October 9 will be watched closely since these altitudes were adopted assuming lower density at higher latitudes. However, they are considered safe to fly based on the new information from T17. The T20 altitude is not planned to be changed. The next two TAMWG meetings are scheduled for September 27 and October 16 after the T18 and T19 flybys.
The Science Operations Plan Update process for S27 kicked off today.
Tuesday, September 12 (DOY 255):
A change board meeting was held today for AACS flight software version A8.7.5. The four parameter changes approved were: secondary safing vector pair update, A and B-branch thruster magnitude updates, Inertial Reference Unit-A scale factor updates, and response script tier count change for a potential fault protection case following an unexpected reaction wheel to thruster transition.
The final approval meeting was held today for the S24 background sequence. The instrument expanded block files will be uplinked beginning today with the background sequence going up on September 18.
The S23 Saturn solar occultation Live Movable Block was successfully uplinked today and has been verified as registered onboard. The file should execute as expected beginning on DOY-258.
The final development process began today for S26. The process will run for ten weeks with uplink of sequence files occurring during the 11th week. S26 begins execution on Friday, November 24.
A beautiful image of Saturn at night is Astronomy Picture of the Day today.
Wednesday, September 13 (DOY 256):
At the time S24 was going through the final development process, Uplink Operations was unable to confirm the DSN allocations requested for the sequence. The uncertainty was part of the STEREO launch and MRO aerobraking conflict that the flight projects have been working with the DSN. Since the allocations were uncertain, SSR data margin that is usually released for instrument use during the development process was withheld, pending possible station losses and the concomitant data cuts that would be required.
Now that the STEREO launch has been shifted to not earlier than October 25, allocations are confirmed for most of S24, but not in time for the instruments to take advantage of the now-available SSR data margin. The S24 leads are handling this by building a mini-sequence to be stored in the movable block region of memory. It will run for most of the sequence from DOY 269 through DOY 291. This file will contain the new data policing table commands, all instrument commands required to take advantage of the sponge bits, and any new instrument expanded block files required which go straight to the instrument, and are not stored on the SSR. The mini-sequence will be uplinked the day after S24 begins execution with a primary window of DOY 264/13:05-18:54, and a backup window of DOY 265/12:50-18:39.
The Magnetospheric and Plasma Science (MAPS) instruments continued the magnetotail campaign to observe plasma flows and the dynamics of the magnetotail from large distances downstream. The spacecraft is entering an important phase of the mission that covers unique geometry optimal for MAPS coverage of the magnetotail and plasma wake.
First viewed at the Saturn Orbit Insertion anniversary event held at JPL for the flight team, the SOI +2 years highlights video chronicles some of Cassini’s discoveries in the last two years. Link to:
Outreach has posted some of the images from the Titan 17 flyby on September 7. To view these images go to:
Check out the Cassini web site at http://saturn.jpl.nasa.gov for the latest press releases and images.
The Cassini-Huygens mission is a cooperative project of NASA, the European Space Agency and the Italian Spsce Agency. The Jet Propulsion Laboratory, a division of the California Institute of Technology in Pasadena, manages the Cassini-Huygens mission for NASA’s Science Mission Directorate, Washington, D.C. JPL designed, developed and assembled the Cassini orbiter.