The interstellar boundary explorer (IBEX): Update at the end of phase B
The Interstellar Boundary Explorer (IBEX) mission will make the first global observations of the heliosphere's interaction with the interstellar medium. IBEX achieves these breakthrough observations by traveling outside of the Earth's magnetosphere in a highly elliptical orbit and taking g...
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Veröffentlicht in: | AIP conference proceedings 2006-01, Vol.858 (1), p.241-250 |
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creator | McComas, D J Allegrini, F Bartolone, L Bochsler, P Bzowski, M Collier, M Fahr, H Fichtner, H Frisch, P Funsten, H Fuselier, Steve Gloeckler, G Gruntman, M Izmodenov, V Knappenberger, P Lee, M Livi, S Mitchell, D Mobius, E |
description | The Interstellar Boundary Explorer (IBEX) mission will make the first global observations of the heliosphere's interaction with the interstellar medium. IBEX achieves these breakthrough observations by traveling outside of the Earth's magnetosphere in a highly elliptical orbit and taking global Energetic Neutral Atoms (ENA) images over energies from ~10 eV to 6 keV. IBEX's high-apogee (~50 RE) orbit enables heliospheric ENA measurements by providing viewing from far above the Earth's relatively bright magnetospheric ENA emissions. This high energy orbit is achieved from a Pegasus XL launch vehicle by adding the propulsion from an IBEX-supplied solid rocket motor and the spacecraft's hydrazine propulsion system. IBEX carries two very large-aperture, single-pixel ENA cameras that view perpendicular to the spacecraft's Sun-pointed spin axis. Each six months, the continuous spinning of the spacecraft and periodic re-pointing to maintain the sun-pointing spin axis naturally lead to global, all-sky images. Over the course of our NASA Phase B program, the IBEX team optimized the designs of all subsystems. In this paper we summarize several significant advances in both IBEX sensors, our expected signal to noise (and background), and our groundbreaking approach to achieve a very high-altitude orbit from a Pegasus launch vehicle for the first time. IBEX is in full scale development and on track for launch in June of 2008. |
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IBEX achieves these breakthrough observations by traveling outside of the Earth's magnetosphere in a highly elliptical orbit and taking global Energetic Neutral Atoms (ENA) images over energies from ~10 eV to 6 keV. IBEX's high-apogee (~50 RE) orbit enables heliospheric ENA measurements by providing viewing from far above the Earth's relatively bright magnetospheric ENA emissions. This high energy orbit is achieved from a Pegasus XL launch vehicle by adding the propulsion from an IBEX-supplied solid rocket motor and the spacecraft's hydrazine propulsion system. IBEX carries two very large-aperture, single-pixel ENA cameras that view perpendicular to the spacecraft's Sun-pointed spin axis. Each six months, the continuous spinning of the spacecraft and periodic re-pointing to maintain the sun-pointing spin axis naturally lead to global, all-sky images. Over the course of our NASA Phase B program, the IBEX team optimized the designs of all subsystems. In this paper we summarize several significant advances in both IBEX sensors, our expected signal to noise (and background), and our groundbreaking approach to achieve a very high-altitude orbit from a Pegasus launch vehicle for the first time. 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IBEX is in full scale development and on track for launch in June of 2008.</description><subject>CAMERAS</subject><subject>EARTH MAGNETOSPHERE</subject><subject>EV RANGE</subject><subject>HELIOSPHERE</subject><subject>HYDRAZINE</subject><subject>KEV RANGE 01-10</subject><subject>NASA</subject><subject>ORBITS</subject><subject>PARTICLE TRACKS</subject><subject>PERIODICITY</subject><subject>PHYSICS OF ELEMENTARY PARTICLES AND FIELDS</subject><subject>PROPULSION</subject><subject>PROPULSION SYSTEMS</subject><subject>ROCKETS</subject><subject>SIGNALS</subject><subject>SOLAR WIND</subject><subject>SPACE VEHICLES</subject><subject>SPIN</subject><issn>0094-243X</issn><issn>1551-7616</issn><isbn>0735403554</isbn><isbn>9780735403550</isbn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2006</creationdate><recordtype>article</recordtype><recordid>eNotj0tLAzEYRYMPsK0u_AcBQXQxNc9J4q4ttRYKblrobsgk39Ap42ScpKD_3pG6uptzL-cidE_JlJKcv9Ap49JwLi7QiEpJM5XT_BKNieJSEC6luEIjQozImOD7GzSO8UgIM0rpEVptD4DrNkEfEzSN7XEZTq23_Q-G764JPfT4aT1f7p9f8a7zNgG2CaehBK3HocLdwUbA81t0Xdkmwt1_TtDubbldvGebj9V6MdtkR0ZJyjx1laxMRfNBy7FS2dKAYrr03BBSOj5IMeuh4rnQCigzXlc5WKKJA5p7PkEP590QU11EVydwBxfaFlwqGNFaMyMG6vFMdX34OkFMxWcd3d-_FsIpFsN5LhUV_Be-xlrD</recordid><startdate>20060101</startdate><enddate>20060101</enddate><creator>McComas, D J</creator><creator>Allegrini, F</creator><creator>Bartolone, L</creator><creator>Bochsler, P</creator><creator>Bzowski, M</creator><creator>Collier, M</creator><creator>Fahr, H</creator><creator>Fichtner, H</creator><creator>Frisch, P</creator><creator>Funsten, H</creator><creator>Fuselier, Steve</creator><creator>Gloeckler, G</creator><creator>Gruntman, M</creator><creator>Izmodenov, V</creator><creator>Knappenberger, P</creator><creator>Lee, M</creator><creator>Livi, S</creator><creator>Mitchell, D</creator><creator>Mobius, E</creator><scope>7U5</scope><scope>8FD</scope><scope>L7M</scope><scope>OTOTI</scope></search><sort><creationdate>20060101</creationdate><title>The interstellar boundary explorer (IBEX): Update at the end of phase B</title><author>McComas, D J ; 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subjects | CAMERAS EARTH MAGNETOSPHERE EV RANGE HELIOSPHERE HYDRAZINE KEV RANGE 01-10 NASA ORBITS PARTICLE TRACKS PERIODICITY PHYSICS OF ELEMENTARY PARTICLES AND FIELDS PROPULSION PROPULSION SYSTEMS ROCKETS SIGNALS SOLAR WIND SPACE VEHICLES SPIN |
title | The interstellar boundary explorer (IBEX): Update at the end of phase B |
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