Doppler shift as Computational Tool, Mars Pathfinder – by Albert Lim

Doppler shifts are common among research in establishing the expanding Universe ( e.g. Hubble ) and the motion of galaxies, rotation of stars, binaries and studies of spectroscopic binaries etc. However, even closer to home, Doppler shift can also be used as powerful computational tools to study the interior of planets as the below example shows.

Mars Pathfinder - Background Information

On 4th December 1996, a Delta II - 7925 launch vehicle with a payload assist module (PAM) propelled the Mars Pathfinder into Earth's orbit and on its 7 month long journey to explore Planet Mars. About 30 hours after launch, Pathfinder will be asked to determine its orientation in space by locating specific stars and adjust its position to be in a direct line of sight to the Earth. A series of 4 Trajectory Correction Manoeuvres or TCMs had also to be performed to put Pathfinder on course to Mars. Tracking, telemetry and command operations were conducted using the Deep Space Network(DSN) - NASA's international network of antennas that supports interplanetary spacecraft missions managed and operated by Jet Propulsion Laboratory (JPL). The DSN essentially consist of 3 deep-space communications facilities placed approximately 120 degrees apart around the world (in California, Spain and Australia) to permit constant link to the spacecraft as the Earth rotates.

On 4th July 1997, Mars Pathfinder - the second of NASA's low cost, quick Discovery class missions, successfully entered the Martian atmosphere, landed and deployed a small rover named Sojourner which explored an area approximately 200 square meters on the surface of Mars. Pathfinder utilise a combination of an 11 meter (36 foot ) parachute, rocket braking systems and air bags to cushion the impact to achieve this historic and novel soft, upright landing at a site in the Ares Vallis region ( 19.33N 33.55W ) at 2.58 am true local solar time.

Pathfinder's lander had operated nearly 3 times its designed lifetime of 30 sols (i.e. Martian days / 1 sol = 24.6 Earth hours ), while the Sojourner rover operated 12 times its designed lifetime of 7 sols on the surface of Mars. Pathfinder collected data from 3 science instruments and 10 technology experiments for nearly 3 months and returned 2.6 billion bits of information ( new data ) including over 16,000 lander and 550 rover images, 16 chemical analyses of rocks and soil and 8.5 million individual temperature, pressure and wind measurements. A record 566 million "hits" were registered during the first month of the mission making the Pathfinder landing by far the largest Internet event in recorded history. The lander has since been named the Sagan Memorial Station in honour of Carl Sagan.
        
The last successful data transmission cycle from Pathfinder was completed at 3.23am Pacific Daylight Time on Sept 27th 1997 which was sol 83 of the mission.
        
Who proposed the use of  Doppler shift as computational tool for Pathfinder ?

Dr. William Folkner, an interdisciplinary scientist at JPL who was part of the Pathfinder Science Team was the first to propose the use of  Doppler measurements and ranging techniques to determine the variations in the rotation of Mars and hence determine properties of its interior and climate.
                          
He proposed studies to determine optimal times for Doppler tracking measurements to be acquired from Mars Pathfinder and modification of software to include Pathfinder tracking data with the earlier Viking lander data combined to establish the precession constant and seasonal rotation variations of Mars.

The Viking lander data has given an estimate of the Martian precession constant with 5% uncertainty and detection of annual rotation-rate variations with 20% uncertainty. Viking results alone Dr. Folkner argued were not accurate enough to place meaningful constraints on the interior structure of Mars. By combining Viking and Pathfinder's new data, the precession constant can be determined to about 1% or better and enable scientist to refine the moment of inertia of Mars and place significant constraints on models for the composition of the mantle. At that time, it should be remembered that the moment of inertia was called “the single most important number about Mars that we don’t know”.

In addition, Doppler tracking data from the lander can be used to investigate possible changes in the gravitation constant G, place tighter constraints on parameters ( such as the PPN parameter γ ) that describe the theory of gravity and to determine masses of some of the asteroids that perturb the orbit of Mars.

What significance is there for Doppler shift data for Pathfinder ?
How can this Doppler shift data from the Doppler Tracker be used ?

Mission scientist can use Doppler shifts in radio communication signals and ranging from Pathfinder to measure the rotation of Mars. This can be achieved through daily Doppler tracking and less frequent 2-way ranging during communication sessions. These can determine the position of the lander to a position of  100 meters - this position can be established to an accuracy a few meters within a few months in the months. The last such positional measurement was done by Viking over 20 years ago. In the meantime, the pole of the planet has undergone precession - that is, the tilt of the planet has wobbled. If the exact location of the Mars Pathfinder lander was known, the orientation and precession rate ( i.e the regular motion or change of the Martian poles with respect to the ecliptic ) can be calculated. These data can then be compared to those of Viking  landers 20 years ago - the difference between the 2 positional measurements should yield the rate of precession. Knowing the precession rate allows scientist to directly calculate the moment of inertia. These provides the constraints ( since it is a function of the distribution of mass within Mars ) scientist are looking for to establish the density of the Martian rock with depth. So indirectly, Doppler computation can provide valuable information about the interior of Mars.

Given 4 parameters, the core size, mass and mantle of Mars can be determined. The combination of Pathfinder Doppler data with earlier data from Viking landers can determine the third parameter - the moment of inertia - through Doppler data calculations to yield Mar’s precession rate. While a forth parameter is needed to complete the interior model, this can be achieved through future Doppler tracking since presence of a fluid core may be detectable through its effects on Mars’ nutation. For now, if Pathfinder can determine the moment of inertia of Mars - it is by itself already a significant constraint on possible models for Mars’ interior.

How Doppler shift data was acquired in Pathfinder mission ?

Because this rotational and orbital dynamics experiment was based on the measuring of Doppler range to the Pathfinder using radio link, Pathfinder was equipped with special 2 way transponder in the X-band.

The Mars Pathfinder utilises the Cassini-designed Deep Space Transponder  (DST). DST is capable of generating 2 way X-band Doppler and range data via the DSN. Two way ( or coherent ) Doppler is produced by measuring the received frequency of the downlink carrier  and comparing it with the uplink carrier frequency which is known and stable. Because the lander moves in relation with the tracking station, the velocity between the two causes  a shift in observed frequency known as Doppler shift - measuring this shift can establish the exact location of the Mars Pathfinder. Typical Doppler noise at X-band is 0.003 - 0.006 Hz for a 60-second count. Similar Doppler techniques are used by the navigation team of Pathfinder to determine the actual trajectory and its orbit for navigational purposes.

In operation, DSN transmit a signal to Pathfinder. The spacecraft tracks the phase of the uplink signal and generates a phase-coherent downlink signal. The DSN then compares the received frequency with the same reference reference frequency from which the uplink was generated. The spacecraft transponder turn around ratios for X band up and down link are 880 / 749 in the below specially allocated frequency range :

                                    X-band uplink         :         7145 - 7190 MHz
                                    X-band downlink     :         8400 - 8440  MHz

DSN reports Doppler data in the form of a continuous phase count which is equivalent to integration of biased Doppler frequency over time.

Mars rotation about its poles causes a signature in the Doppler data with a daily minimum when the lander is closest to the Earth. Changes in daily signature reveal information about the planet’s interior through its effect of precession and nutation.

Outcome from Doppler Tracking / rotational and orbital dynamics experiment

Daily Doppler tracking and two way ranging during communications sessions provided data to calculate very precise position of the lander. These allow calculation of precession rate  and the moment of inertia of Mars. The calculated precession rate is consistent with the hypothesis that the non-hydrostatic component of inertia at 0.3653 + / - 0.0056 and is due to the Tharsis bulge.

From Pathfinder’s determination of the moment of inertia, we know that Mars must have a central metallic core of between 1,300 and 2,400 km in radius.
        
We know also know that if the iron-enriched Sherottite meteorites are typical of the mantle composition of Mars, then the mantle must be warmer than Earth’s at the same pressure levels. Scientist for the first time now can put constraints on interior temperatures of Mars.

Pathfinder also detected an annual variation in the planet’s rotation rate which can be explained by the seasonal exchange of carbon dioxide between the atmosphere and the ice caps.

Long term signatures in Doppler data were detected and attributed to perturbations caused by asteroids. The masses of asteroids were also calculated and determined from Pathfinder Doppler data.

Because of Pathfinder, scientist can now also understand how Mars has evolved over time much better. This was expressed clearly by Dr. David Baltimore who is president of the California Institute of Technology which manages JPL for NASA. I am confident astronomers from all over the world would agree to that.

 
 

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