Phoenix (spacecraft): Difference between revisions
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[[Image:Phoenix-Medium.jpg|thumb|right|300px|PHOTO CREDIT:NASA - KENNEDY SPACE CENTER, FLA. -- On Launch Pad 17-A at Cape Canaveral Air Force Station, the Phoenix Mars Lander waits for the fairing installation. NASA/George Shelton]] |
[[Image:Phoenix-Medium.jpg|thumb|right|300px|PHOTO CREDIT:NASA - KENNEDY SPACE CENTER, FLA. -- On Launch Pad 17-A at Cape Canaveral Air Force Station, the Phoenix Mars Lander waits for the fairing installation. NASA/George Shelton]] |
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[[Image:Phoenix KSC-07PD-2115.jpg|thumb|right|300px|PHOTO CREDIT: NASA - On Launch Pad 17-A at Cape Canaveral Air Force Station, the first half of the fairing is moved into place around the Phoenix Mars Lander for installation.]] |
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Revision as of 00:31, 30 July 2007
This Delta II 7925 with the Phoenix spacecraft, 3 August 2007 at 09:35 GMT documents a current or recent spaceflight. Details may change as the mission progresses. Initial news reports may be unreliable. The last updates to this Delta II 7925 with the Phoenix spacecraft, 3 August 2007 at 09:35 GMT may not reflect the most current information. For more information please see WikiProject Spaceflight. |
- For the Star Trek spacecraft, see Phoenix (Star Trek). For other uses of Phoenix, see Phoenix
![](http://upload.wikimedia.org/wikipedia/commons/thumb/8/8f/Phoenix_lander_illustration_2006.jpg/300px-Phoenix_lander_illustration_2006.jpg)
![](http://upload.wikimedia.org/wikipedia/commons/thumb/6/66/Phoenix-Medium.jpg/300px-Phoenix-Medium.jpg)
![](http://upload.wikimedia.org/wikipedia/commons/thumb/e/e7/Phoenix_KSC-07PD-2115.jpg/300px-Phoenix_KSC-07PD-2115.jpg)
Phoenix is a robotic spacecraft which will be used for a space exploration mission to Mars. The scientists conducting the mission will use instruments aboard the Phoenix lander to search for environments suitable for microbial life on Mars, and to research the history of water there. Phoenix is scheduled to launch on August 3 2007[1], and land on Mars in May 2008. The multi-agency program is headed by the Lunar and Planetary Laboratory at the University of Arizona, under the direction of NASA. The program is a partnership of universities from the US, Canada, Switzerland and Germany, NASA, the Canadian Space Agency, and the aerospace industry. Phoenix will land in the planet's water-ice-rich northern polar region and will use its robotic arm to dig into the arctic terrain.[2]
History
In August 2003 NASA selected the University of Arizona "Phoenix" mission for launch in 2007 as what is hoped will be the first in a new line of smaller, low-cost, "Scout" missions in the agency's exploration of Mars program[3]. The selection was the result of an intense two-year competition with proposals from other institutions. The $325 million NASA award is more than six times larger than any other single research grant in University of Arizona history.
Peter H. Smith of the University of Arizona Lunar and Planetary Laboratory, was selected to lead the mission as Principal Investigator. The mission was named after the Phoenix, a mythological bird that is repeatedly reborn of ashes. Like the mythological bird, the 2007 Phoenix contains several previously built components. The lander used for the 2007 mission is the modified Mars Surveyor 2001 Lander (cancelled in 2000), along with several of the instruments from both that and the previous polar lander mission. Lockheed Martin had kept the nearly-complete lander in environmentally-controlled storage since 2001.
![](http://upload.wikimedia.org/wikipedia/commons/thumb/7/79/Phoenix_Mars_Lander_in_testing_PIA01885.jpg/220px-Phoenix_Mars_Lander_in_testing_PIA01885.jpg)
Phoenix is a partnership of universities, NASA centers, and the aerospace industry. The science instruments and operations will be a University of Arizona responsibility. NASA's Jet Propulsion Laboratory in Pasadena, California, will manage the project and provide mission design and control. Lockheed Martin Space Systems, Denver, Colorado, will build and test the spacecraft. The Canadian Space Agency will provide a meteorological station, including an innovative laser-based atmospheric sensor. The Co-Investigator institutions include Malin Space Science Systems (California), Max Planck Institute for Solar System Research (Germany), NASA Ames Research Center (California), NASA Johnson Space Center (Texas), Optech Incorporated, SETI Institute, Texas A&M University, Tufts University, University of Colorado, University of Michigan, University of Neuchâtel (Switzerland), University of Texas at Dallas, University of Washington, Washington University in St. Louis, and York University (Canada).
On June 2 2005, following a critical review of the project's planning progress and preliminary design, NASA approved the mission to proceed as planned[4]. The purpose of the review was to confirm NASA's confidence in the mission.
The lander will land the same way the Viking program landers did, slowed primarily by landing rockets. In 2007, a report was filed to the American Astronomical Society by Washington State University professor Dirk Schulze-Makuch that made a claim that rocket exhaust contaminated the Viking landing sites, potentially killing any life that may have been there.[5] The hypothesis was made long after any modifications to Phoenix could be made without delaying the mission significantly. One of the investigators on the Phoenix mission, NASA astrobiologist Chris McKay, merely stated that the report "piqued his interest". Experiments conducted by Nilton Renno, mission Co-Investigator from the University of Michigan, and his students have specifically looked at how much surface dust will be kicked up when Phoenix lands.[6]
Launch
![](http://upload.wikimedia.org/wikipedia/commons/thumb/2/24/Wikinews-logo.svg/40px-Wikinews-logo.svg.png)
Phoenix is scheduled to launch on 3 August 2007 at 5:35:18 a.m. EDT (09:35:18 UTC) on a Delta 7925 launch vehicle. The spacecraft was scheduled to arrive at Pad 17-A of the Cape Canaveral Air Force Station on July 23.[7] NASA expects the launch will take place during a launch window which extends from 3 August to 25 August, 2007. Due to the small launch window the rescheduled launch of the Dawn mission (originally planned for the 7 July) had to stand down and will launch after Phoenix in September. The Delta 7925 was chosen due to its successful launch history, which includes launches of the Spirit and Opportunity Mars Exploration Rovers in 2003 and Mars Pathfinder in 1996.[8]
Mission
The mission has two goals. One is to study the geologic history of water, the key to unlocking the story of past climate change. The second is to search for evidence of a habitable zone that may exist in the ice-soil boundary, the "biological paydirt". The Phoenix's instruments are suitable for uncovering information on the geological and possibly biological history of the Martian Arctic. Because the Phoenix will be the first mission to return data from either of the poles, it will contribute to NASA's main strategy for Mars exploration, "Follow the water".
The primary mission is anticipated to last 90 sols.
Scientific payload
Phoenix will carry improved versions of University of Arizona panoramic cameras and volatiles-analysis instrument from the ill-fated Mars Polar Lander, as well as experiments that had been built for the Mars Surveyor 2001 Lander, including a JPL trench-digging robot arm and a chemistry-microscopy instrument. The science payload also includes a descent imager and a suite of meteorological instruments.[9]
Robotic Arm (RA)
The Robotic Arm is designed to extend 2.35 m from its base on the lander, and have the ability to trench up to half a meter below the surface. It will take samples of dirt and water-ice that will be analyzed with other instruments on the lander. The arm was designed and built for the Jet Propulsion Laboratory by Alliance Spacesystems, LLC in Pasadena California. Alliance has delivered both the engineering model and flight versions of the arm to JPL for testing and integration.
Robotic Arm Camera (RAC)
![](http://upload.wikimedia.org/wikipedia/commons/2/2f/Phoenix_Spacecraft_ra_cam.jpg)
The Robotic Arm Camera will be attached to the Robotic Arm, just above the scoop. It will be a full-color camera, which will be able to take pictures of the area, as well as verify the samples that the scoop will return, and will be able to examine the grains of the area where the Robotic Arm has just dug up. The camera is being made by the University of Arizona and Max Planck Institute, Germany.
Surface Stereo Imager (SSI)
![](http://upload.wikimedia.org/wikipedia/commons/d/d8/Phoenix_Spacecraft_ssi.jpg)
The Surface Stereo Imager will be the primary camera on the spacecraft. It is a stereo camera that is described as "a higher resolution upgrade of the imager used for Mars Pathfinder and the Mars Polar Lander"[10]. It is expected to take many stereo images of the Martian Arctic. It will also be able, using the Sun as a reference, to measure the atmospheric distortion of the Martian atmosphere due to dust and air and other features. The camera is being provided by the University of Arizona in collaboration with the Max Planck Institute for Solar System Research. [11] [12]
Thermal and Evolved Gas Analyzer (TEGA)
![](http://upload.wikimedia.org/wikipedia/commons/4/4a/Phoenix_Spacecraft_tega.jpg)
TEGA is a combination of a high-temperature furnace with a mass spectrometer. It will be used to bake samples of Martian dust, and determine the content of this dust. It has 8 different ovens, each about the size of a large ball-point pen, which will be able to analyze one sample each, for a total of 8 different samples. Team members can measure how much water vapor and carbon dioxide gas are given off, how much water-ice the samples contain, and what minerals are present that may have formed during a wetter, warmer past climate. The instrument will also be capable of measuring any organic volatiles, up to 10 ppb. TEGA is being built by the University of Arizona and University of Texas at Dallas. [13]
Mars Descent Imager (MARDI)
![](http://upload.wikimedia.org/wikipedia/commons/4/4e/Phoenix_Spacecraft_MARDI.jpg)
The Mars Descent Imager will be used to take a picture of the Martian soil as the lander descends. As originally planned, it would have begun taking pictures after the aeroshell departed, about 5 miles above the Martian soil. Before launch, testing uncovered a potential problem with hardware that would have handled the image data. As a result, mission planners decided to take just one photograph with MARDI.[14] Hopefully this one image can still help pinpoint exactly where the lander has landed, and possibly help find potential science targets. It will also be used to learn if the area where the lander lands is typical of the surrounding terrain. MARDI was built by Malin Space Science Systems.[15]
MARDI will be the lightest camera ever to land on Mars, as well as the most efficient. It only uses 3 watts of power during the imaging process, as compared to the many watts used by most other space cameras.
Microscopy, Electrochemistry, and Conductivity Analyzer (MECA)
![](http://upload.wikimedia.org/wikipedia/commons/e/e8/Phoenix_Spacecraft_Meca.jpg)
MECA is a combination of a wet chemistry lab, optical and atomic force microscope, and a thermal and electrical conductivity probe[16]. It is being built by the Jet Propulsion Laboratory.
Using this instrument, researchers will examine soil particles as small as 16 micrometres across. They will measure electrical and thermal conductivity of soil particles using a probe on the robotic arm scoop. One of the most interesting experiments is the wet chemistry laboratory.
The robotic arm will scoop up some soil, put it in one of four wet chemistry lab cells, where water will be added, and while stirring, an array of electrochemical sensors will measure a dozen dissolved ions such as sodium, magnesium, calcium, and sulfate in the water, that have leached out from the soil. This is important, because it will give us information as the biological compatibility of the soil, both for possible indigenous microbes and for future Earth visitors. Sensors will also measure the pH and conductivity of the soil-water mixture, telling us if the wet soil is super acidic or alkaline and salty, or full of oxidants that can destroy life.
Meteorological Station (MET)
![](http://upload.wikimedia.org/wikipedia/commons/thumb/2/24/Wikinews-logo.svg/40px-Wikinews-logo.svg.png)
MET will record the daily weather during the course of the Phoenix Mission. It is equipped with a variety of temperature and pressure sensors to do so. It is also equipped with LIDAR, or Laser Imaging Detection and Ranging, which will be used to find the amount and number of dust particles in the air. It is being built by the Canadian Space Agency in cooperation with scientists at Dalhousie University.
The Phoenix DVD
Attached to the deck of the lander is The Phoenix DVD[1] compiled by the Planetary Society. The disc contains Visions from Mars[2], a multimedia collection of literature and art about the Red Planet. Works include the text of H.G. Wells' War of the Worlds (and its infamous radio broadcast by Orson Welles), Percival Lowell's Mars as the Abode of Life with a map of his proposed canals, Bradbury's The Martian Chronicles, and Kim Stanley Robinson's Green Mars. There are also messages directly addressed to future Martian visitors or settlers from, among others, Carl Sagan and Arthur C. Clarke. In the Fall of 2006, The Planetary Society collected a quarter million names submitted through the internet and placed them on the disc, which claims, on the front, to be "the first library on Mars".
The Phoenix DVD is made of a special silica glass that can purportedly withstand the Martian environment, lasting for hundreds (if not thousands) of years on the surface while it awaits discoverers.
Engineering information
The Phoenix Lander is being built by Lockheed Martin. Most of its parts were built for the cancelled Mars Surveyor 2001 Lander. It was then locked away in a clean room for several years, until the mission was funded by the NASA Scout Program. [17]
While many of the parts are being used from the previous spacecraft, many are being updated. The lander contains the following subsystems:
- A computer system for commanding the spacecraft and handling data
- An electrical system containing solar arrays and batteries
- A telecommunications system that can communicate directly with earth, as well as Mars Odyssey and the Mars Reconnaissance Orbiter
- A sophisticated guidance system to ensure the spacecraft will land successfully
- A propulsion system to land safely consisting of 6 hydrazine engines.
- The structure of the spacecraft
- Several mechanical systems to move parts of the spacecraft
- A sophisticated thermo-control system to ensure the spacecraft does not get too cold.
See also
References
- ^ "NASA Launch Schedule". NASA. Retrieved 2006-07-24.
- ^ Phoenix Mars Scout (wikisource)
- ^ "Mars 2007 'Phoenix' will Study Water near Mars' North Pole" August 4, 2003 NASA Press release. URL accessed April 2, 2006
- ^ "NASA's Phoenix Mars Mission Begins Launch Preparations" - June 2, 2005 NASA Press release. URL accessed April 2, 2006
- ^ ""Did probes find Martian life ... or kill it off?"". Associated Press via MSNBC. 2007-01-08. Retrieved 2007-05-31.
{{cite web}}
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suggested) (help) - ^ "Expendable Launch Vehicle Status Report". NASA. 07.13.07.
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(help) - ^ "Phoenix Mars Mission - Launch". University of Arizona.
- ^ Shotwell R. (2005). "Phoenix—the first Mars Scout mission�". Acta Astronautica. 57: 121–134. doi:10.1016/j.actaastro.2005.03.038.
{{cite journal}}
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at position 37 (help) - ^ "Phoenix Mars Lander- SSI". Phoenix Mars Lander. Retrieved 2006-04-02.
- ^ P. H. Smith, R. Reynolds, J. Weinberg, T. Friedman, M. T. Lemmon, R. Tanner, R. J. Reid, R. L. Marcialis, B. J. Bos, C. Oquest, H. U. Keller, W. J. Markiewicz, R. Kramm,F. Gliem and P. Rueffer (2001). "The MVACS Surface Stereo Imager on Mars Polar Lander" (PDF). Journal of Geophysical Research. 106 (E8): 17, 589–17, 607.
{{cite journal}}
: CS1 maint: multiple names: authors list (link) - ^ Reynolds R.O.,Smith P.H., Bell L.S., Keller, H.U. (2001). "The design of Mars lander cameras for Mars Pathfinder, MarsSurveyor '98 and Mars Surveyor '01". IEEE Transactions on Instrumentation and Measurement. 50 (1): 63–71. doi:10.1109/19.903879.
{{cite journal}}
: CS1 maint: multiple names: authors list (link) - ^ Boynton, W. V.; Quinn, R. C. (2005). "Thermal and Evolved Gas Analyzer: Part of the Mars Volatile and Climate Surveyor integrated payload". Journal of Geophysical Research. 106 (E8): 17683–17698. doi:10.1029/1999JE001153.
{{cite journal}}
: CS1 maint: multiple names: authors list (link) - ^
"One image planned during descent of Phoenix". The University of Arizona. July 3, 2007.
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(help) - ^
Malin, M. C.; Caplinger, M. A.; Carr, M. H.; Squyres, S.; Thomas, P.; Veverka, J. (2005). "Mars Descent Imager (MARDI) on the Mars Polar Lander" (PDF). 106: 17635–17650. doi:10.1029/1999JE001144.
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suggested) (help)CS1 maint: multiple names: authors list (link) - ^ "Spacecraft and Science Instruments". Phoenix Mars Lander. Retrieved 2007-03-10.
- ^ "Phoenix Mars Lander- Spacecraft". Phoenix Mars Lander. Retrieved 2006-06-09.
External links
![](http://upload.wikimedia.org/wikipedia/en/thumb/4/4a/Commons-logo.svg/30px-Commons-logo.svg.png)