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| [[File:Pioneer 10-11 - P50 - fx.jpg|thumb|right|Helium Vector Magnetometer (HVM) of [[Pioneer 10]] and [[Pioneer 11|11]] spacecraft]]
| | The main advantage of using the blog is that anyone can use the Word - Press blog and customize the elements in the theme regardless to limited knowledge about internet and website development. You can either install Word - Press yourself or use free services offered on the web today. The effect is to promote older posts by moving them back onto the front page and into the rss feed. Hosted by Your Domain on Another Web Host - In this model, you first purchase multiple-domain webhosting, and then you can build free Wordpress websites on your own domains, taking advantage of the full power of Wordpress. Understanding how Word - Press works can be a challenge, but it is not too difficult when you learn more about it. <br><br>Always remember that an effective linkwheel strategy strives to answer all the demands of popular search engines while reacting to the latest marketing number trends. Some of the Wordpress development services offered by us are:. It sorts the results of a search according to category, tags and comments. t need to use the back button or the URL to get to your home page. Akismet is really a sophisticated junk e-mail blocker and it's also very useful thinking about I recieve many junk e-mail comments day-to-day across my various web-sites. <br><br>Usually, Wordpress owners selling the ad space on monthly basis and this means a residual income source. Note: at a first glance WP Mobile Pro themes do not appear to be glamorous or fancy. This platform can be customizedaccording to the requirements of the business. These frequent updates have created menace in the task of optimization. Premium vs Customised Word - Press Themes - Premium themes are a lot like customised themes but without the customised price and without the wait. <br><br>If you enjoyed this short article and you would such as to get additional facts concerning [http://uto.1admin.name/wordpress_backup_plugin_3785160 backup plugin] kindly go to our webpage. The disadvantage is it requires a considerable amount of time to set every thing up. This plugin allows a webmaster to create complex layouts without having to waste so much time with short codes. When we talk about functional suitability, Word - Press proves itself as one of the strongest contestant among its other rivals. If you are looking for Hire Wordpress Developer then just get in touch with him. It does take time to come up having a website that gives you the much needed results hence the web developer must be ready to help you along the route. <br><br>You will know which of your Word - Press blog posts are attracting more unique visitors which in turn will help you develop better products and services for your customers. It can run as plugin and you can still get to that whole database just in circumstance your webhost does not have a c - Panel area. Word - Press can also be quickly extended however improvement API is not as potent as Joomla's. Word - Press is the most popular personal publishing platform which was launched in 2003. Verify whether your company has a team of developers or programmers having hands-on experience and knowledge about all Word - Press concepts. |
| '''Spacecraft magnetometers''' are [[magnetometer]]s used aboard [[spacecraft]] and [[satellites]], mostly for scientific investigations, plus [[Flight dynamics|attitude sensing]]. Magnetometers are among the most widely used [[scientific instrument]]s in exploratory and observation satellites. These instruments were instrumental in the discovery of the [[Van Allen radiation belt]]s around Earth by [[Explorer 1]], and have detailed the [[magnetic fields]] of the [[Earth]], [[Moon]], [[Sun]], [[Mars]], [[Venus]] and other planets. There are ongoing missions using magnetometers,{{such as?}} including attempts to define the shape and activity of [[Saturn]]'s core.
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| The first spacecraft-borne magnetometer was placed on the [[Sputnik 3]] spacecraft in 1958 and the most detailed magnetic observations of the Earth have been performed by the [[Magsat]]<ref>[http://www-ssc.igpp.ucla.edu/personnel/russell/ESS265/History.html History of Vector Magnetometers in Space]</ref> and [[Ørsted (satellite)|Ørsted]] satellites. Magnetometers were taken to the Moon during the later [[Apollo 16|Apollo]] missions. Many instruments have been used to measure the strength and direction of [[magnetic field line]]s around Earth and the [[solar system]].
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| Spacecraft magnetometers basically fall into three categories: fluxgate, search-coil and [[ionized]] gas magnetometers. The most accurate magnetometer complexes on spacecraft contain two separate instruments, with a [[helium]] ionized gas magnetometer used to calibrate the fluxgate instrument for more accurate readings. Many later magnetometers contain small ring-coils oriented at 90° in two dimensions relative to each other forming a triaxial framework for indicating direction of magnetic field.
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| ==Magnetometer types==
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| Magnetometers for non-space use evolved from the 19th to mid-20th centuries, and were first employed in spaceflight by Sputnik 3 in 1958. A main constraint on magnetometers in space is the availability of power and mass. Magnetometers fall into 3 major categories: the fluxgate type, search coil and the ionized vapor magnetometers. The newest type is the [[Nuclear Overhauser effect|Overhauser type]] based on [[nuclear magnetic resonance]] technology.
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| ===Fluxgate magnetometers===
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| [[Image:Mars global surveyor.jpg|thumb|right|300px|magnetometers are mounted at both ends of the solar panel assemblies to isolate them from the spacecraft's magnetic fields]]
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| Fluxgate magnetometers are used for their electronic simplicity and low weight. There have been several types of fluxgate used in spacecraft, which vary in two regards. Primarily better readings are obtained with three magnetometers, each pointing in a different direction. Some spacecraft have instead achieved this by rotating the craft and taking readings at 120° intervals, but this creates other issues. The other difference is in the configuration, which is simple and circular.
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| Magnetometers of this type were equipped on the "[[Pioneer 0]]"/Able 1, "[[Pioneer 1]]"/Able 2, Ye1.1, Ye1.2, and Ye1.3 missions that failed in 1958 due to launch problems. The Pioneer 1 however did collect data on the Van Allen belts.<ref name="deep space chronicle">Asif A. Siddiqi [http://history.nasa.gov/monograph24/1958.pdf 1958. Deep space chronicle. A Chronology of Deep Space and Planetary Probes 1958–2000] History. NASA.</ref> In 1959 the Soviet "[[Luna 1]]"/Ye1.4 carried a three-component magnetometer that passed the moon en route to a heliocentric orbit at a distance of {{convert|6400|mi|km}}, but the magnetic field could not be accurately assessed.<ref name="deep space chronicle"/> Eventually the USSR managed a lunar impact with "[[Luna 2]]", a three component magnetometer, finding no significant magnetic field in close approach to the surface.<ref name="deep space chronicle"/> Explorer 10 had an abbreviated 52 hr mission with two fluxgate magnetometers on board. During 1958 and 1959 failure tended to characterize missions carrying magnetometers: 2 instruments were lost on [[Pioneer P-3|Able IVB]] alone. In early 1966 the [[USSR]] finally placed [[Luna 10]] in orbit around the moon carrying a magnetometer and was able to confirm the weak nature of the moon's magnetic field.<ref name="deep space chronicle"/> [[Venera 4]], [[Venera 5|5]], and [[Venera 6|6]] also carried magnetometers on their trips to [[Venus]], although they were not placed on the landing craft.
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| [[Image:Lunar Prospector orbiter.jpg|thumb|left|[[Lunar Prospector]] probe, the magnetometer is mounted on the boom-end facing toward the viewer]]
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| ====Vector sensors====
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| The majority of early fluxgate magnetometers on spacecraft were made as vector sensors. However, the magnetometer electronics created [[harmonic]]s which interfered with readings. Properly designed sensors had feedback electronics to the detector that effectively neutralized the harmonics. [[Mariner 1]] and [[Mariner 2]] carried fluxgate-vector sensor devices. Only Mariner 2 survived launch and as it passed Venus on December 14, 1962 it failed to detect a magnetic field around the planet. This was in part due to the distance of the spacecraft from the planet, noise within the magnetometer, and a very weak Venusian magnetic field.<ref name="deep space chronicle"/> Pioneer 6, launched in 1965, is one of 4 Pioneer satellites circling the sun and relaying information to Earth about solar winds. This spacecraft was equipped with a single vector-fluxgate magnetometer.<ref name="deep space chronicle"/>
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| ====Ring core and spherical====
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| Ring core sensor fluxgate magnetometers began replacing vector sensor magnetometers with the [[Apollo 16]] mission in 1972, where a three axis magnetometer was placed on the moon. These sensors were used on a number of satellites including [[Magsat]], [[Voyager program|Voyager]], [[Ulysses (spacecraft)|Ulysses]], [[Giotto mission|Giotto]], [[Active Magnetospheric Particle Tracer Explorers|AMPTE]]. The [[Lunar Prospector]]-1 uses ring-coil made of these alloys extended away from each other and its spacecraft to look for remnant magnetism in the moons 'non-magnetic' surface.<ref>[http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1998-001A-05 Lunar Prospector Magnetometer (MAG)] National Space Science Data Center, NASA</ref><ref name="pmid9727968">{{cite journal |author=Konopliv AS, Binder AB, Hood LL, Kucinskas AB, Sjogren WL, Williams JG |title=Improved gravity field of the moon from lunar prospector |journal=Science |volume=281 |issue=5382 |pages=1476–80 |date=September 1998 |pmid=9727968 |doi= 10.1126/science.281.5382.1476|url=http://www.sciencemag.org/cgi/pmidlookup?view=long&pmid=9727968|bibcode = 1998Sci...281.1476K }}</ref>[[Image:MGS Fluxgate Magnetometer.png|thumb|300px|Wiring diagram and picture of the Magnetometer used on Mars Global Surveyor]] Properly configured, the magnetometers are capable of measuring magnetic field differences of 1 nT. These devices, with cores about 1 cm in size, were of lower weight than vector sensors. However, these devices were found to have non-linear output with magnetic fields greater than >5000 nT. Later is was discovered that creating a spherical structure with feedback loops wire transverse to the ring in the sphere could negate this effect. These later magnetometers were called spherical fluxgate or compact spherical core (CSC) magnetometers used in the [[Ørsted (satellite)|Ørsted satellite]]. The metal alloys that form the core of these magnetometers has also improved since Apollo-16 mission with latest using advanced [[Permalloy|molybdenum-permalloy]] alloys, producing lower noise with more stable output.<ref>[http://mgs-mager.gsfc.nasa.gov/instrument.html The MGS Magnetometer and Electron Reflectometer] Mars global surveyor, NASA</ref>
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| [[Image:Search coil magnetometer.png|thumb|left|Photograph of the search coil magnetometers used on the THEMIS and Cluster/Staff mission.]]
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| ===Search-coil magnetometer===
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| '''[[Search coil|Search-coil magnetometers]]''', also called induction magnetometers, are wound coils around a core of high magnetic permeability. Search coils concentrate magnetic field lines inside the core along with fluctuations.<ref>[http://www.nasa.gov/mission_pages/themis/spacecraft/SCM.html Search Coil Magnetometers (SCM)] THEMIS mission. NASA</ref> The benefit of these magnetometers is that they measure alternating magnetic field and so can resolve changes in magnetic fields quickly, many times per second. Following [[Lenz's law]], the voltage is proportional to the time derivative of magnetic flux. The voltage will be amplified by the apparent permeability of the core. This apparent permeability (µa) is defined as: | |
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| <math>\ {\mu}_a= \frac \mu{1+N\mu} </math>.
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| The [[Pioneer 5]] mission finally managed to get a working magnetometer of this type in orbit around the sun showing that magnetic fields existed between Earth and Venus orbits.<ref name="deep space chronicle"/><ref>[http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1960-001A-02 Magnetometer - Pioneer 5 mission]</ref> A single magnetometer was oriented along the plane perpendicular to the spin axis of the spacecraft. Search coil magnetometers have become increasingly more common in Earth observation satellites. A commonly used instrument is the triaxial search-coil magnetometer. [[Orbiting Geophysical Observatory]] (OGO missions - [[OGO-1]] to [[OGO-6]])<ref>[http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1964-054A-01 Search coil magnetometer - OGO1 mission] , National Space Science Data Center, NASA</ref><ref>Frandsen, A. M. A., Holzer, R. E., and Smith, E. J. ''OGO Search Coil Magnetometer Experiments''. (1969) IEEE Trans. Geosci. Electron. GE-7, 61-74.</ref> The [[Vela (satellite)]] mission used this type as part of a package to determine if nuclear weapons evaluation was being conducted outside earth's atmosphere.<ref>[http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1964-040A-08 Search coil magnetometers - Vela2A mission] National Space Science Data Center, NASA</ref> In September 1979 a Vela satellite collected evidence of [[Vela Incident|a potential nuclear burst]] over the South Western Indian Ocean. In 1997 the US created the [[Fast Auroral Snapshot Explorer|FAST]] that was designed to investigate aurora phenomena over the poles.<ref>[http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1996-049A-04 Tri-Axial Fluxgate and Search-coil Magnetometers - FAST Mission] National Space Science Data Center, NASA</ref> And currently it is investigating magnetic fields at 10 to 30 Earth radii with the THEMIS satellites<ref>[http://nssdc.gsfc.nasa.gov/nmc/spacecraftDisplay.do?id=2007-004A Search coil magnetometer - Themis-A] National Space Science Data Center, NASA</ref> THEMIS, which stands for ''Time History of Events and Macroscale Interactions during Substorms'' is an array of five satellites which hope to gather more precise history of how magnetic storms arise and dissipate.<ref>[http://nssdc.gsfc.nasa.gov/nmc/spacecraftDisplay.do?id=2007-004A Themis-A] National Space Science Data Center, NASA</ref>
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| ===Ionized gas magnetometers===
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| ====Heavy metal — scalar====
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| Certain spacecraft, like [[Magsat]], are equipped with '''scalar magnetometer'''. The output of these device, often in out frequency, is proportional to the magnetic field. The Magsat and [[Grm-A1]] had '''cesium-vapor''' (cesium-133) sensor heads of dual-cell design, this design left two small dead zones. [[Explorer 10]] (P14) was equipped with a rubidium vapor magnetometer, presumably a scalar magnetometer since the spacecraft also had a fluxgate. The magnetometer was fouled accidentally which caused it to overheat, it worked for a period of time but 52 h into the mission transmission went dead and was not regained.<ref>[http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1961-010A-01 RB-Vapor and Fluxgate Magnetometers] National Space Science Data Center, NASA</ref> Ranger 1 and 2 carried a rubidium vapor magnetometer, failed to reach lunar orbit.<ref name="deep space chronicle"/>
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| ====Helium====
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| This type of magnetometer depends on the variation in helium absorptivity, when excited, polarized infrared light with an applied magnetic field.<ref>[http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1967-060A-05 Triaxial Low Field Helium Magnetometer - Mariner 5 mission] National Space Science Data Center, NASA</ref> A low field vector-helium magnetometer was equipped on the [[Mariner 4]] spacecraft to Mars like the Venus probe a year earlier, no magnetic field was detected.<ref>[http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1964-077A-02 Helium Magnetometer-Mariner 4 mission] National Space Science Data Center, NASA</ref> [[Mariner 5]] used a similar device For this experiment a low-field helium magnetometer was used to obtain triaxial measurements of interplanetary and Venusian magnetic fields. Similar in accuracy to the triaxial flux-gated magnetometers this device produced more reliable data.
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| ===Other types===
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| '''[[Magnetometer#Overhauser_magnetometer|Overhauser magnetometer]]''' provides extremely accurate measurements of the strength of the [[magnetic field]]. The [[Orsted (satellite)]] uses this type of magnetometer to map the magnetic fields over the surface of the earth.
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| On the [[Vanguard 3]] mission (1959) a '''proton processional magnetometer''' was used to measure geomagnetic fields. The proton source was hexane.<ref>[http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1959-007A-01 Proton Processional Magnetometer] National Space Science Data Center, NASA</ref>
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| ==Configurations of magnetometers==
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| Unlike ground based magnetometers that can be oriented by the user to determine the direction of magnetic field, in space the user is linked by telecommunications to a satellite traveling at 25,000 km per hour. The magnetometers used need to give an accurate reading quickly to be able to deduce magnetic fields. Several strategies can be employed, it is easier to rotate a space craft about its axis than to carry the weight of an additional magnetometer. Other strategy is to increase the size of the rocket, or make the magnetometer lighter and more effective. One of the problems, for example in studying planets with low magnetic fields like Venus, does require more sensitive equipment. The equipment has necessarily needed to evolve for today's modern task. Ironically satellites launched more the 20 years ago still have working magnetometers in places where it would take decades to reach today, at the same time the latest equipment is being used to analyze changes in the Earth here at home.
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| ===Uniaxial===
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| These simple fluxgate magnetometers were used on many missions. On [[Pioneer 6]] and [[Injun 1]] the magnetometers were mounted to a bracket external to the space craft and readings were taken as the spacecraft rotated every 120°.<ref>[http://nssdc.gsfc.nasa.gov/nmc/experimentSearch.do?spacecraft=Pioneer%20%206 Uniaxial Fluxgate Magnetometer - Pioneer 6] National Space Science Data Center, NASA</ref> [[Pioneer 7]] and [[Pioneer 8]] are configured similarly.<ref>[http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1967-123A-01 Single-Axis Magnetometer-Pioneer 9] National Space Science Data Center, NASA</ref> The fluxgate on [[Explorer 6]] was mounted along the spin axis to verify spacecraft tracking magnetic field lines. Search coil magnetometers were used on [[Pioneer 1]], Explorer 6, [[Pioneer 5]], and [[Deep Space 1]].
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| ===Diaxial===
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| A two axis magnetometer was mounted to the [[ATS-1]] (Applications Technology Satellite).<ref>[http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1966-110A-02 Biaxial Fluxgate Magnetometer - Application Technology Satellite -1 (ATS-1)] National Space Science Data Center, NASA</ref> One sensor was on a 15 cm boom and the other on the spacecraft's spin axis (Spin stabilized satellite). The sun was used to sense the position of the boom mounted device, and triaxial vector measurements could be calculated. Compared to other boom mounted magnetometers, this configuration had considerable interference. Interestingly with this spacecraft, the sun induce magnetic oscillations and this allowed the continued use of the magnetometer after the sun sensor failed. Explorer 10 had two fluxgate magnetometers but is technically classified as a dual technique since it also had a rubidium vapor magnetometer.
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| ===Triaxial===
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| The [[Sputnik]]-3 had a '''vector fluxgate''' magnetometer, however because the orientation of the spacecraft could not be determined the direction vector for the magnetic field could not be determined. Three axis magnetometers were used on [[Luna 1]], [[Luna 2]], [[Pioneer Venus]], [[Mariner 2]], [[Venera 1]], [[Explorer 12]], [[Explorer 14]], and [[Explorer 15]]. [[Explorer 33]] was 'to be' the first US spacecraft to enter stable orbit around the moon was equipped with the most advanced magnetometer, a boom-mounted triaxial fluxgate (GFSC) magnetometer of the early-vector type. It had a small range but was accurate to a resolution of 0.25 nT.<ref>[http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1966-058A-01 GFSC Magnetometer - Explorer 33] National Space Science Data Center, NASA</ref> However after a rocket failure it was left in a highly elliptical orbit around Earth that orbited through the electro/magnetic tail.<ref>Behannon KW. ''Mapping of the Earth's Bow Shock and Magnetic Tail by Explorer 33. 1968. J. Geophys. Res. 73: 907-930</ref> [[Image:Apollo 16 ALSEP-TAFGMAG.PNG|thumb|left|Image of the lunar stationed magnetometer as part of the ALSEP package]] The [[Pioneer 9]] and [[Explorer 34]] used a configuration similar to Explorer 33 to survey the magnetic field within Earth's solar orbit. [[Explorer 35]] was the first of its type to enter stable orbit around the moon, this proved important because with the sensitive triaxial magnetometer on board, it was found the moon effectively had no magnetic field, no radiation belt, and solar winds directly impacted the moon.<ref name="deep space chronicle"/> [[Lunar Prospector]] surveyed for surface magnetism around the moon (1998–99), using the triaxial (extended) magnetometers. With Apollo 12 improved magnetometers were placed on the moon as part of the [[Lunar Module]]/[[Apollo Lunar Surface Experiments Package]]
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| (ALSEP).<ref>[http://nssdc.gsfc.nasa.gov/nmc/spacecraftDisplay.do?id=1969-099C Lunar Surface Magnetometer - Apollo-12 Lunar module] National Space Science Data Center, NASA</ref><ref>[http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1969-099C-04 Lunar Surface Magnetometer] National Space Science Data Center, NASA</ref> The magnetometer continued to work several months after that return module departed. As part of the [[Apollo 14]] ALSEP, there was a portable magnetometer.
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| The first use of the three axis ring-coil magnetometer was on the [[Apollo 16]] moon mission. Subsequently is was used on the [[Magsat]]. The [[MESSENGER]] mission has triaxial ring-coil magnetometer with a range of +/- 1000 mT and a sensitivity of 0.02 mT, still in progress, the mission is designed to get detailed information about Mercurian magnetosphere.<ref>[http://nssdc.gsfc.nasa.gov/nmc/spacecraftDisplay.do?id=2004-030A MESSENGER] Space Science Data Center, NASA]</ref> The first use of spherical magnetometer in three axis configuration was on the [[Orsted (satellite)]].
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| [[Image:Magnetic Field Earth.png|thumb|right|300px|Modeled Earth magnetic fields, data created by satellites with sensitive magnetometers]]
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| ===Dual technique===
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| Each type of magnetometer has its own built in 'weakness'. This can result from the design of the magnetometer to the way the magnetometer interacts with the spacecraft, radiation from the sun, resonances, etc. Using completely different design is a way to measure which readings are the result of natural magnetic fields and the sum of magnetic fields altered by spacecraft systems.
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| In addition each type has its strengths. The fluxgate type is relatively good at providing data that finds magnetic sources. One of the first Dual technique systems was the abbreviated [[Explorer 10]] mission which used a rubidium vapor and biaxial fluxgate magnetometers. Vector helium is better at tracking magnetic field lines and as a scalar magnetometer. [[Cassini–Huygens|Cassini spacecraft]] used a '''Dual Technique Magnetometer'''. One of these devices is the ring-coil vector fluxgate magnetometer (RCFGM). The other device is a vector/scalar helium magnetometer.<ref>[http://saturn.jpl.nasa.gov/spacecraft/instruments-cassini-mag.cfm SPACECRAFT - Cassini Orbiter Instruments - MAG]</ref> The RCFGM is mounted 5.5 m out on an 11 m boom with the helium device at the end.
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| [[Explorer 6]] (1959) used a search coil magnetometer to measure the gross magnetic field of the Earth and vector fluxgate.,<ref>[http://nssdc.gsfc.nasa.gov/nmc/experimentSearch.do?spacecraft=Explorer%20%206 Experiments Explorer 6] National Space Science Data Center, NASA</ref> however because of induced magnetism is the space craft the fluxgate sensor became saturated and did not send data. Future missions would attempt to place magnetometers further away from the space craft.
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| Magsat Earth geological satellite was also Dual Technique. This satellite and Grm-A1 carried a scalar cesium vapor magnetometer and vector fluxgate magnetometers.<ref>[http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1979-094A-01 Scalar Magnetometer [[Magsat]] mission] National Space Science Data Center, NASA</ref><ref>[http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=1979-094A-02 Vector Magnetometer [[Magsat]] mission] National Space Science Data Center, NASA</ref> The Grm-A1 satellite carrier the magnetometer on 4 meter boom. This particular spacecraft was designed to hold in a precised equi-gravitational orbit, while taking measurements.<ref>[http://nssdc.gsfc.nasa.gov/nmc/spacecraftDisplay.do?id=GRM-A1 GRM-A1] National Space Science Data Center, NASA
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| </ref> For purposes similar to Magsat, the [[Orsted_%28satellite%29#Instruments|Ørsted]] satellite, also used a dual technique system. The [[Magnetometer#Overhauser magnetometer|Overhauser magnetometer]] is situated at the end of an 8 meter long boom, in order to minimize disturbances from the satellite's electrical systems. The CSC fluxgate magnetometer is located inside the body and associated with a star tracking device. One of the greater accomplishments of the two missions, the Magsat and Orsted missions happen to capture a period of great magnetic field change, with the potential of a loss of dipole, or pole reversal.<ref name="pmid11948347">{{cite journal |author=Hulot G, Eymin C, Langlais B, Mandea M, Olsen N |title=Small-scale structure of the geodynamo inferred from Oersted and Magsat satellite data |journal=Nature |volume=416 |issue=6881 |pages=620–3 |date=April 2002 |pmid=11948347 |doi=10.1038/416620a |url=|bibcode = 2002Natur.416..620H }}</ref><ref>[http://www.nasa.gov/centers/goddard/news/topstory/2004/0517magnet.html NASA AND USGS MAGNETIC DATABASE "ROCKS" THE WORLD] NASA Web Feature, NASA</ref>
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| ===By Mounting===
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| The simplest magnetometer implementations are mounted directly to their vehicles. However, this places the sensor close to potential interferences such as vehicle currents and ferrous materials. For relatively insensitive work, such as "compasses" (attitude sensing) in [[Low Earth orbit]], this may be sufficient.
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| The most sensitive magnetometer instruments are mounted on long booms, deployed away from the craft (e.g., [[Voyager program|the Voyagers]], [[Cassini-Huygens|Cassini]]). Many contaminant fields then [[Inverse-square law|decrease strongly with distance]], while background fields appear unchanged. Two magnetometers may be mounted, one only partially down the boom. The vehicle body's fields will then appear different at the two distances, while background fields may or may not change significantly over such scales. Magnetometer booms for vector instruments must be rigid, to prevent additional flexing motions from appearing in the data.
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| Some vehicles mount magnetometers on simpler, existing appendages, such as specially-designed solar arrays (e.g., [[Mars Global Surveyor]], [[Juno (spacecraft)|Juno]]. This saves the cost and mass of a separate boom. However, a solar array must have its cells carefully implemented and tested to avoid becoming a [[Electromagnet|contaminating field]].
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| ==See also==
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| [[Magnetorquer]]
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| ==References==
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| {{reflist}}
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| {{Satellite and spacecraft instruments}}
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| [[Category:Spacecraft components]]
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The main advantage of using the blog is that anyone can use the Word - Press blog and customize the elements in the theme regardless to limited knowledge about internet and website development. You can either install Word - Press yourself or use free services offered on the web today. The effect is to promote older posts by moving them back onto the front page and into the rss feed. Hosted by Your Domain on Another Web Host - In this model, you first purchase multiple-domain webhosting, and then you can build free Wordpress websites on your own domains, taking advantage of the full power of Wordpress. Understanding how Word - Press works can be a challenge, but it is not too difficult when you learn more about it.
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You will know which of your Word - Press blog posts are attracting more unique visitors which in turn will help you develop better products and services for your customers. It can run as plugin and you can still get to that whole database just in circumstance your webhost does not have a c - Panel area. Word - Press can also be quickly extended however improvement API is not as potent as Joomla's. Word - Press is the most popular personal publishing platform which was launched in 2003. Verify whether your company has a team of developers or programmers having hands-on experience and knowledge about all Word - Press concepts.