Mars Pathfinder
Mission type | Lander · Rover |
---|---|
Operator | NASA · Jet Propulsion Laboratory |
COSPAR ID | 1996-068A |
SATCAT no. | 24667 |
Website | mars |
Mission duration | 85 days Launch to last contact: 9 months, 23 days |
Spacecraft properties | |
Launch mass | 890 kg (includes propellant)[2] |
Power | Pathfinder: 35 W Sojourner: 13 W |
Start of mission | |
Launch date | December 4, 1996 SLC-17 | 06:58:07
Contractor | None[3] |
End of mission | |
Last contact | September 27, 1997UTC | 10:23
AMT | |
Landing site | Ares Vallis, Chryse Planitia, Mars 19°7′48″N 33°13′12″W / 19.13000°N 33.22000°W |
Transponders | |
Band | X-Band with high-gain antenna |
Bandwidth | 6 kb/s to 70 m Deep Space Network, 250 b/s to surface command[2] |
Official insignia of the Mars Pathfinder mission. Discovery program → |
Mars Pathfinder
Launched on December 4, 1996, by
This mission was the first of a series of missions to Mars that included rovers, and was the first successful lander since the two
In addition to scientific objectives, the Mars Pathfinder mission was also a "proof-of-concept" for various technologies, such as
Mission objectives
- To prove that the development of "faster, better and cheaper" spacecraft was possible (with three years for development and a cost under $150 million for the lander, and $25 million for the rover[6]).
- To show that it was possible to send a load of scientific instruments to another planet with a simple system and at one-fifteenth the cost of a Viking mission. (For comparison, the Viking missions cost $935 million in 1974[7] or $3.5 billion in 1997 dollars.)
- To demonstrate NASA's commitment to low-cost planetary exploration by finishing the mission with a total expenditure of $280 million, including the launch vehicle and mission operations.
Science experiments
The Mars Pathfinder conducted different investigations on the Martian soil using three scientific instruments. The lander contained a stereoscopic camera with spatial filters on an expandable pole called Imager for Mars Pathfinder (IMP),[8][9] and the Atmospheric Structure Instrument/Meteorology Package (ASI/MET)[10] which acted as a Mars meteorological station, collecting data about pressure, temperature, and winds. The MET structure included three windsocks mounted at three heights on a pole, the topmost at about one meter (3.3 ft) and generally registered winds from the West.[11]
The
The rover was equipped with three CCD cameras, all manufactured by Eastman Kodak Company and controlled by the rover's CPU. The two front-facing monochrome cameras served navigation purposes and were coupled with five laser stripe projectors for stereoscopic hazard detection. These front cameras had a resolution of 484 vertical by 768 horizontal pixels, and an optical resolution capable of discerning details as small as 0.6 cm (0.24 in) across a range of 0.65 m (26 in). Images from these cameras could be compressed using the block truncation coding (BTC) algorithm.
The third camera, situated at the rear near the APXS, was used for color imaging. It shared the resolution of the front cameras but was rotated 90 degrees to capture images of both the APXS target area and the rover's tracks. This rear camera featured a 4x4 pixel block with specific color sensitivities: 12 pixels for green, two for red, and two for
Pathfinder lander
Imager for Mars Pathfinder (IMP), (includes magnetometer and anemometer)[14][15]
The IMP had a set of filters designed to record surface and atmospheric phenomena. There were two cameras, or eyes, allowing for stereoscopic imagery, with the set of filters being slightly different between them. [16][17][18]
Eye and Filter | Center Wavelength (nm) | Bandwidth (nm) | Category |
---|---|---|---|
L0 | 443 | 26 | Stereo, Geology |
L5 | 671 | 20 | Stereo, Geology |
L6 | 802 | 21 | Geology |
L7 | 858 | 34 | Geology |
L8 | 898 | 41 | Geology |
L9 | 931 | 27 | Stereo, Ranging, Geology |
L10 | 1003 | 29 | Geology |
L11 | 968 | 31 | Stereo, Ranging, Geology |
R0 | 443 | 26 | Stereo, Geology |
R5 | 671 | 20 | Stereo, Geology |
R6 | 752 | 19 | Geology |
R8 | 600 | 21 | Geology |
R9 | 531 | 30 | Stereo, Ranging, Geology |
R10 | 480 | 27 | Geology |
R11 | 967 | 30 | Stereo, Ranging, Geology |
L1 | 450 | 5 | Solar |
L2 | 883 | 6 | Solar |
L3 | 925 | 5 | Solar |
L4 | 935 | 5 | Solar |
R1 | 670 | 5 | Solar |
R2 | 946 | 44 | Solar |
R3 | 936 | 5 | Solar |
R4 | 989 | 5 | Solar |
Atmospheric and meteorological sensors (ASI/MET)
The ASI/MET recorded temperature, pressure and wind data, during entry and descent, and once on the surface.[16] It also housed electronics for sensor operation and data recording.[16]
Sojourner rover
- Imaging system (three cameras: front B&W stereo,[13] 1 rear color)
- Laser striper hazard detection system[19]
- Alpha Proton APXS)
- Wheel Abrasion Experiment
- Materials Adherence Experiment
- Accelerometers
Landing site
The landing site was an ancient flood plain in Mars's northern hemisphere called "Ares Vallis" ("the valley of Ares", the ancient Greek equivalent of the ancient Roman deity Mars) and is among the rockiest parts of Mars. Scientists chose it because they found it to be a relatively safe surface to land on and one that contained a wide variety of rocks deposited during a catastrophic flood. After the landing, at 19°08′N 33°13′W / 19.13°N 33.22°W,[20] succeeded, the lander received the name The Carl Sagan Memorial Station in honor of the astronomer.[21] (See also List of extraterrestrial memorials)
Entry, descent and landing
Mars Pathfinder entered the Martian atmosphere and landed using an innovative system involving an entry capsule, a supersonic parachute, followed by solid rockets and large airbags to cushion the impact.
Mars Pathfinder directly entered Mars atmosphere in a retrograde direction from a hyperbolic trajectory at 6.1 km/s (14,000 mph) using an atmospheric entry aeroshell (capsule) that was derived from the original Viking Mars lander design. The aeroshell consisted of a back shell and a specially designed ablative heatshield to slow to 370 m/s (830 mph) where a supersonic disk-gap-band parachute was inflated to slow its descent through the thin Martian atmosphere to 68 m/s (150 mph). The lander's on-board computer used redundant on-board accelerometers to determine the timing of the parachute inflation. Twenty seconds later the heatshield was pyrotechnically released. Another twenty seconds later the lander was separated and lowered from the backshell on a 20 m (66 ft) bridle. When the lander reached 1.6 km (5,200 ft) above the surface, a radar was used by the on-board computer to determine altitude and descent velocity. This information was used by the computer to determine the precise timing of the landing events that followed.[22]
Once the lander was 355 m (1,165 ft) above the ground, airbags were inflated in less than a second using three gas generators.[23] The airbags were made of four inter-connected multi-layer vectran bags that surrounded the tetrahedron lander. They were designed and tested to accommodate grazing angle impacts as high as 28 m/s (63 mph). However, as the airbags were designed for no more than about 15 m/s (34 mph) vertical impacts, three solid retrorockets were mounted above the lander in the backshell.[24] These were fired at 98 m (322 ft) above the ground. The lander's on-board computer estimated the best time to fire the rockets and cut the bridle so that the lander velocity would be reduced to about zero between 15 and 25 m (49 and 82 ft) above the ground. After 2.3 seconds, while the rockets were still firing, the lander cut the bridle loose about 21.5 m (71 ft) above the ground and fell to the ground. The rockets flew up and away with the backshell and parachute (they have since been sighted by orbital images). The lander impacted at 14 m/s (31 mph) and limited the impact to only 18 G of deceleration. The first bounce was 15.7 m (52 ft) high and continued bouncing for at least 15 additional bounces (accelerometer data recording did not continue through all of the bounces).[25]
The entire entry, descent and landing process was completed in four minutes.
Once the lander stopped rolling, the airbags deflated and retracted toward the lander using four winches mounted on the lander "petals". Designed to right itself from any initial orientation, the lander happened to roll right side up onto its base petal. Eighty-seven minutes after landing, the petals were deployed with Sojourner rover and the solar panels attached on the inside.[26]
The lander arrived at night at 2:56:55 Mars local solar time (16:56:55 UTC) on July 4, 1997. The lander had to wait until sunrise to send its first digital signals and images to Earth. The landing site was located at 19.30° north latitude and 33.52° west longitude in Ares Vallis, only 19 km (12 mi) southwest of the center of the 200 km (120 mi) wide landing site ellipse. During Sol 1, the first Martian solar day the lander spent on the planet, the lander took pictures and made some meteorological measurements. Once the data was received, the engineers realized that one of the airbags had not fully deflated and could be a problem for the forthcoming traverse of Sojourner's descent ramp. To solve the problem, they sent commands to the lander to raise one of its petals and perform additional retraction to flatten the airbag. The procedure was a success and on Sol 2, Sojourner was released, stood up and backed down one of two ramps.[26]
Rover operations
Sojourner deployment
The Sojourner rover departed from the lander on Sol 2, after its landing on July 4, 1997. As the next sols progressed it approached some rocks, which the scientists named "
characters. The rover made measurements of the elements found in those rocks and in the martian soil, while the lander took pictures of the Sojourner and the surrounding terrain, in addition to making climate observations.The Sojourner is a six-wheeled, 65 cm (26 in) long vehicle, 48 cm (19 in) wide, 30 cm (12 in) tall and weighing 10.5 kg (23 lb).[27] Its maximum speed reached 1 cm/s (0.39 in/s). Sojourner travelled approximately 100 m (330 ft) in total, never more than 12 m (39 ft) from the Pathfinder station. During its 83 sols of operation, it sent 550 photographs to Earth and analyzed the chemical properties of 16 locations near the lander. (See also Space exploration rovers)
Sojourner's rock analysis
The first analysis on a rock started on Sol 3 with Barnacle Bill. The
The APXS works by irradiating rocks and soil samples with alpha particles (helium nuclei, which consist of two protons and two neutrons). The results indicated that "Barnacle Bill" is much like Earth's andesites, confirming past volcanic activity. The discovery of andesites shows that some Martian rocks have been remelted and reprocessed. On Earth, andesite forms when magma sits in pockets of rock while some of the iron and magnesium settle out. Consequently, the final rock contains less iron and magnesiums and more silica. Volcanic rocks are usually classified by comparing the relative amount of alkalis (Na2O and K2O) with the amount of silica (SiO2). Andesite is different from the rocks found in meteorites that have come from Mars.[28][29][30]
Analysis of the Yogi rock again using the APXS showed that it was a basaltic rock, more primitive than Barnacle Bill. Yogi's shape and texture show that it was probably deposited there by a flood.
Another rock, named Moe, was found to have certain marks on its surface, demonstrating erosion caused by the wind. Most rocks analyzed showed a high content of
By the time that final results of the mission were described in a series of articles in the journal Science (December 5, 1997), it was believed that the rock Yogi contained a coating of dust, but was similar to the rock Barnacle Bill. Calculations suggest that the two rocks contain mostly the minerals orthopyroxene (magnesium-iron silicate), feldspars (aluminum silicates of potassium, sodium, and calcium), and quartz (silicon dioxide), with smaller amounts of magnetite, ilmenite, iron sulfide, and calcium phosphate.[28][29][30]
On-board computer
The
The computer of the Pathfinder lander was a Radiation Hardened IBM Risc 6000 Single Chip (Rad6000 SC) CPU with 128 MB of RAM and 6 MB of EEPROM[33][34] and its operating system was VxWorks.[35]
The mission was jeopardised by a concurrent software bug in the lander,[36] which had been found in preflight testing but was deemed a glitch and therefore given a low priority as it only occurred in certain unanticipated heavy-load conditions, and the focus was on verifying the entry and landing code. The problem, which was reproduced and corrected from Earth using a laboratory duplicate thanks to the logging and debugging functionality enabled in the flight software, was due to computer resets caused by priority inversion. No scientific or engineering data was lost after a computer reset, but all the following operations were interrupted until the next day.[37][38] Four resets occurred (on July 5, 10, 11 and 14) during the mission,[39] before patching the software on July 21 to enable priority inheritance.[40]
Results from Pathfinder
The lander sent more than 2.3 billion bits (287.5 megabytes) of information including 16,500 pictures and made 8.5 million measurements of the atmospheric pressure, temperature and wind speed.[41]
By taking multiple images of the sky at different distances from the Sun, scientists were able to determine that the size of the particles in the pink haze was about one
Using
End of mission
Although the mission was planned to last from a week to a month, the rover operated successfully for almost three months. Communication failed after October 7,[45] with a final data transmission received from Pathfinder at 10:23 UTC on September 27, 1997. Mission managers tried to restore full communications during the following five months, but the mission was terminated on March 10, 1998. During the extended operation a high-resolution stereo panorama of the surrounding terrain was being made, and the Sojourner rover was to visit a distant ridge, but the panorama was only about one-third completed and the ridge visit had not begun when communication failed.[45]
The on-board battery—designed to operate for one month—may have failed after repeated charging and discharging. The battery was used to heat the probe's electronics to slightly above the expected nighttime temperatures on Mars. With the failure of the battery, colder-than-normal temperatures may have caused vital parts to break, leading to loss of communications.[45][46] The mission had exceeded its goals in the first month.
Mars Reconnaissance Orbiter spotted the Pathfinder lander in January 2007 (see photo).[47][48]
Naming the rover
The name Sojourner was chosen for the Mars Pathfinder rover when 12-year old Valerie Ambroise, of Bridgeport, Connecticut, won a year-long, worldwide competition in which students up to 18 years old were invited to select a heroine and submit an essay about her historical accomplishments. The students were asked to address in their essays how a planetary rover named for their heroine would translate these accomplishments to the Martian environment.
Initiated in March 1994 by The Planetary Society of Pasadena, California, in cooperation with NASA's Jet Propulsion Laboratory (JPL), the contest got under way with an announcement in the January 1995 issue of the National Science Teachers Association's magazine Science and Children, circulated to 20,000 teachers and schools across the nation.[49]
Ambroise's winning essay, which suggested naming the rover for the 19th century women's rights activist
Honors
- In 1997, the Sojourner Team was awarded a JPL Award for Technical Excellence
- On October 21, 1997, at the Salt Lake City, Utah, Sojourner was awarded honorary membership in the Planetary Geology Division of the society[51]
- In 2003, Sojourner was inducted into the Robot Hall of Fame
In popular culture
- The opening title sequence of the television series Star Trek: Enterprise features footage of Sojourner on the Martian surface, intermixed with various other images representative of humankind's evolution of air and space flight.
- In the 2000 film Red Planet, astronauts stranded on Mars make a makeshift radio from parts of Pathfinder, and use it to communicate with their spaceship.
- In the 2011 novel The Martian by Andy Weir, and its 2015 film adaptation, the protagonist, Mark Watney, who is stranded alone on Mars, travels to the long-dead Pathfinder site (noting the "Twin Peaks" as a landmark in the novel), and returns it to his base in an attempt to communicate with Earth.[52]
Sojourner's location in context
See also
- Exploration of Mars – Overview of the exploration of Mars
- Life on Mars – Scientific assessments on the microbial habitability of Mars
- List of missions to Mars
- Mars Exploration Rover – NASA mission to explore Mars via two rovers
- Mars Science Laboratory – Robotic mission that deployed the Curiosity rover to Mars in 2012
- Mars 2020 – Astrobiology Mars rover mission by NASA
- Comparison of embedded computer systems on board the Mars rovers
Notes
- ^ a b Nelson, Jon. "Mars Pathfinder / Sojourner Rover". NASA. Archived from the original on February 19, 2014. Retrieved February 2, 2014.
- ^ a b "Mars Pathfinder Fact Sheet". NASA/JPL. March 19, 2005. Archived from the original on September 19, 2014. Retrieved February 21, 2014.
- ^ Conway, Erik (2015). "The Discovery Program: Mars Pathfinder". Jet Propulsion Laboratory. Archived from the original on January 17, 2015. Retrieved June 10, 2015.
- ^ "Mars Pathfinder". NASA. Archived from the original on November 12, 2011. Retrieved June 10, 2015.
- Washington Post. Retrieved March 6, 2023.
- ^ "Mars Pathfinder Rover". National Aeronautics and Space Administration. Retrieved September 30, 2020.
- ^ Ezell, Edward Clinton; Ezell, Linda Neuman (1984). "Viking Lander: Building A Complex Spacecraft - Reorganizations and Additional Cutbacks". On Mars: Exploration of the Red Planet 1958-1978. Washington, D.C.: National Aeronautics and Space Administration. pp. 268–270. Archived from the original on April 8, 2016. Retrieved June 10, 2015.
- .
- PMID 9388170.
- PMID 9388169.
- ^ "Windsocks on Mars". JPL/NASA Mars Pathfinder. 2005. Archived from the original on March 5, 2016. Retrieved June 10, 2015.
- .
- ^ a b "Rover Camera Instrument Description". NASA. Archived from the original on March 5, 2016. Retrieved June 10, 2015.
- ^ "IMP Camera Specifications". mars.nasa.gov. Retrieved March 29, 2023.
- ^ .
- ^ a b c "Mars Pathfinder Instrument Descriptions". mars.nasa.gov. Retrieved March 29, 2023.
- ^ a b "How does the IMP work ?". mars.nasa.gov. Retrieved March 29, 2023.
- ^ a b "IMP Instrument Overview" (PDF). atmos.nmsu.edu.
- hdl:2014/25424.
- ^ "Mars Pathfinder Science Results". NASA. Archived from the original on September 20, 2008. Retrieved June 9, 2008.
- ^ "Mars lander renamed for Sagan". NASA. Archived from the original on December 11, 2018. Retrieved September 5, 2017.
- ^ "Mars Pathfinder - Entry Descent and Landing". mars.nasa.gov. Retrieved February 16, 2021.
- USGS. Retrieved March 31, 2021.
- ^ "Rocket Assisted Descent – The RAD Rocket Motors". mars.nasa.gov. Retrieved February 16, 2021.
- ISSN 0022-4650.
- ^ a b "NASA – NSSDCA – Spacecraft – Details". nssdc.gsfc.nasa.gov. Retrieved February 16, 2021.
- ^ "Mars – the search for life" (PDF). NASA. March 4, 2009. Archived from the original (PDF) on March 27, 2009. Retrieved March 28, 2009.
- ^ a b c Golombek, M. et al. 1997. "Overview of the Mars Pathfinder Mission and Assessment of Landing Site Predictions". Science. Science: 278. pp. 1743–1748
- ^ a b "APXS Composition Results". NASA. Archived from the original on June 3, 2016. Retrieved June 10, 2015.
- ^ Bibcode:2001LPI....32.1293B.
- ^ "Mars Pathfinder FAQs - Sojourner CPU". NASA. Archived from the original on December 29, 2014. Retrieved June 10, 2015.
- (PDF) from the original on March 4, 2016. Retrieved June 10, 2015.
- ^ ""QUESTION: What type of computer is the Pathfinder utilizing? ..." (NASA Quest Q&A)". NASA. 1997. Archived from the original on March 7, 2016. Retrieved July 21, 2015.
- ^ ""QUESTION: When it was designed, why was only a single 80C85 CPU used? ..." (NASA Quest Q&A)". NASA. 1997. Archived from the original on July 23, 2015. Retrieved July 21, 2015.
- ^ "Wind River Powers Mars Exploration Rovers—Continues Legacy as Technology Provider for NASA's Space Exploration". Wind River Systems. June 6, 2003. Archived from the original on January 6, 2010. Retrieved August 28, 2009.
- ^ Parallel sparking: Many chips make light work, Douglas Heaven, New Scientist magazine, issue 2930, August 19, 2013, p44. Online (by subscription) Archived October 6, 2014, at the Wayback Machine
- ^ Reeves, Glenn E. (December 15, 1997). "What really happened on Mars? – Authoritative Account". Microsoft.com. Archived from the original on June 11, 2015. Retrieved June 10, 2015.
- ^ Jones, Michael B. (December 16, 1997). "What really happened on Mars?". Microsoft.com. Archived from the original on June 12, 2015. Retrieved June 10, 2015.
- ^ "The Mars Pathfinder Mission Status Reports — Second Week". Office of the Flight Operations Manager – Mars Pathfinder Project. Archived from the original on January 4, 2016. Retrieved October 24, 2015.
- ^ "The Mars Pathfinder Mission Status Reports — Third Week". Office of the Flight Operations Manager – Mars Pathfinder Project. Archived from the original on April 10, 2016. Retrieved October 24, 2015.
- ^ "Mars Pathfinder and Sojourner". NASA. Archived from the original on June 23, 2015. Retrieved June 10, 2015.
- ^ Smith, P. et al. 1997. "Results from the Mars Pathfinder Camera" Science: 278. 1758–1765
- ^ Hviid, S. et al. 1997. "Magnetic Properties Experiments on the Mars Pathfinder Lander: Preliminary Results". Science:278. 1768–1770.
- ^ Bertelsen, P. et al. 2004. "Magnetic Properties Experiments on the Mars Exploration rover Spirit at Gusev Crater". Science: 305. 827–829.
- ^ a b c "Mars Pathfinder Nearing Its End". sciencemag.org. Archived from the original on June 21, 2013. Retrieved June 10, 2015.
- ^ "NASA facts - Mars Pathfinder" (PDF). Jet Propulsion Laboratory. Archived (PDF) from the original on May 13, 2013. Retrieved September 30, 2013.
- ^ McKee, Maggie (January 12, 2007). "Mars probe may have spotted lost rover". New Scientist. Archived from the original on April 24, 2015. Retrieved September 4, 2017.
- ^ "Mars Pathfinder Landing Site and Surroundings". NASA. Archived from the original on May 20, 2015. Retrieved June 10, 2015.
- ^ "NASA Names First Rover to Explore the Surface of Mars". NASA. Archived from the original on June 7, 2011. Retrieved November 29, 2010.
- ^ "Pathfinder Rover Gets Its Name". NASA. Archived from the original on May 27, 2015. Retrieved June 10, 2015.
- ^ "Division Activity at Recent Meetings" (PDF). Planetary Geology Division Newsletter. 16 (1): 1. 1997. Archived from the original (PDF) on June 8, 2011.
- ISBN 978-0-8041-3902-1.
References
- This article draws heavily on the corresponding article in the Spanish-language Wikipedia, which was accessed in the version of March 28, 2005.
- JPL Mars Pathfinder article
- Mars Pathfinder Litograph Set, NASA. (1997)
- Poster: Mars Pathfinder –Roving the Red Planet, NASA. (1998)
- Deep Space Chronicle: A Chronology of Deep Space and Planetary Probes 1958–2000, Asif A. Siddiqi. Monographs in Aerospace History, #24. June 2002, NASA History Office.
- "Return to Mars", article by William R. Newcott. National Geographic, pp. 2–29. Vol. 194, 2nd edition – August 1998.
- "La misión Pathfinder –rebautizada Carl Sagan Memorial Station, en memoria del célebre astrónomo-, paso a paso todo Marte", de J. Roberto Mallo. Conozca Más, págs. 90–96. Edición número 106 – agosto de 1997.
- "Un espía que anda por Marte", de Julio Guerrieri. Descubrir, págs. 80–83. Edición número 73 – agosto de 1997.
- "Mars Pathfinder: el inicio de la conquista de Marte" EL Universo, Enciclopedia de la Astronomía y el Espacio, Editorial Planeta-De Agostini, págs. 58–60. Tomo 5. (1997)
- Sojourner: An Insider's View of the Mars Pathfinder Mission, by ISBN 0-425-19199-0
- Experiences with operations and autonomy of the Mars Pathfinder microrover, A. H. Mishkin, J. C. Morrison, T. T. Nguyen, H. W. Stone, B. K. Cooper and B. H. Wilcox. In Proceedings of the IEEE Aerospace Conference, Snowmass, CO 1998.