Mars Express To Provide Support For Phoenix Landing
Beginning late on 25 May, Mars Express will execute a series of pre-programmed commands specially designed to support NASA’s Phoenix lander. The ESA spacecraft will conduct a high-speed slew, enabling it to track Phoenix as it enters the Martian atmosphere.
Mars Express will point its Lander Communications Antenna toward Phoenix’s planned entry trajectory and record signals transmitted from the lander as it plunges toward the surface during the critical entry, descent and landing (EDL) phase.
Support for Phoenix starts at 21:00 CEST when the spacecraft’s MELACOM (Mars Express Lander Communications) system is switched on. Recording of radio signals transmitted by Phoenix will begin at 01:21 CEST, 26 May and end at 01:47 CEST, 26 May.
During the recording, Mars Express will conduct a high-speed slew as MELACOM tracks Phoenix, keeping Phoenix in the line of sight of the MELACOM antenna.
Upon completion of recording, Mars Express will perform a (normal) slew to Earth pointing attitude, and at 02:25 CEST on 26 May, the spacecraft will begin transmitting the recorded data, via a NASA deep-space ground station, to ESA’s Space Operations Centre (ESOC), Darmstadt, Germany. The one-way signal travel time will be 15 minutes and 20 seconds. The download will be complete by 02:57 CEST, and ESOC will make the data available to NASA immediately upon receipt.
Mars Express will subsequently download the recorded data two more times to ensure redundancy. The ESA spacecraft will additionally monitor signals from Phoenix during an overflight of the landing zone, 08:12-08:23 CEST, and 14 more times during the following week. During the night of 25/26 May, Mars Express will be controlled by the Flight Control Team working in the Dedicated Control Room at ESOC.
Observations before and during Phoenix descent
It is planned that two Mars Express instruments, the High Resolution Stereo Camera (HRSC) and the Ultraviolet and Infrared Atmospheric Spectrometer (SPICAM), will be turned on for observations during the Phoenix EDL.
The observations are aimed at visually capturing the trail of the lander’s trajectory to the Martian surface, studying the characteristics of the atmosphere during the lander’s descent, and monitoring the lander’s performance during EDL.
It is not possible to know the exact route Phoenix will take when descending to the surface, and so it is possible that the instruments may not be looking in the correct direction during the event. This makes the likelihood of success less than certain.
Nonetheless, and despite the technical and physical challenges, the Mars Express science teams are doing their best to boost the potential scientific value of the observations. In any event, highest priority will be given to tracking the lander using MELACOM.
These challenging scientific observations have never been performed at Mars before, and if successful, the knowledge gained will be useful for future missions.
In addition to the observations planned during EDL, the Planetary Fourier Spectrometer (PFS) on board Mars Express has been collecting relevant data since 8 May this year. This includes information on the physical conditions of the Martian atmosphere (temperature, pressure and density) above the expected the landing site. This data is being provided to NASA in support of their observations of the physical conditions in the atmosphere prior to landing.
Timeline Notes (see graph)
# S/C = spacecraft
# CEST = UTC + 2 hours
# Earth time = spacecraft event time + 15:20 min:sec
# MEX: Mars Express | PHX: Phoenix | O/F: Overflight | DSS: Deep space station
# All times subject to change. For latest times relevant to Phoenix, see NASA Phoenix website.
Image 1: Mars Express left Earth for Mars on a six-month journey in June 2003, when the positions of the two planets made for the shortest possible route, a condition that occurs once every twenty-six months. The intrepid spacecraft was launched from the Baikonur Cosmodrome in Kazakhstan onboard a Russian Soyuz/Fregat launcher. It completed the interplanetary cruise, achieving a velocity of 10 800 km/h relative to Earth, in December 2003. Five days before arrival, Mars Express released the Beagle 2 lander, which was subsequently lost. Since entering its operational, near-polar orbit, Mars Express has operated perfectly, delivering some of the most spectacular and scientifically valuable results ever received from the Red Planet. Credits: ESA – Illustration by Medialab
VIDEO: Animation showing artist’s impression of Phoenix during the entry, descent and landing (EDL) phase on 26 May 2008. At the request of NASA, ESA’s Mars Express monitored radio signals from Phoenix using the MELACOM lander communication system, originally intended for use with the Beagle lander. The recorded data will serve as a useful and potentially crucial back-up to compare Phoenix’s planned and actual descent profiles. Landing is planned for 23:38 UTC, 25 May, which is 01:38 CEST, 26 May. Credits: NASA/JPL, Solar System Visualization and Daniel Maas, Maas Digital LLC Download Options Here