The PLANET-B mission

Abstract PLANET-B is the Japanese Mars orbiter program. The spacecraft will begin its journey to Mars in July 1998, and will be inserted into Mars orbit in October 1999. It will collect data for at least one Martian year (about two Earth years). The primary objective of the program is to study the M...
Ausführliche Beschreibung

Gespeichert in:

Autor*in:	Yamamoto, T. [verfasserIn] Tsuruda, K. [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	1998

Schlagwörter:	Solar Wind Solar Zenith Angle Parking Orbit Mars Orbit Martian Ionosphere

Anmerkung:	© The Society of Geomagnetism and Earth, Planetary and Space Sciences (SGEPSS); The Seismological Society of Japan; The Volcanological Society of Japan; The Geodetic Society of Japan; The Japanese Society for Planetary Sciences. 1998

Übergeordnetes Werk:	Enthalten in: Earth, planets and space - Springer Berlin Heidelberg, 1998, 50(1998), 3 vom: März, Seite 175-181
Übergeordnetes Werk:	volume:50 ; year:1998 ; number:3 ; month:03 ; pages:175-181

Links:	Volltext

DOI / URN:	10.1186/BF03352100

Katalog-ID:	SPR036894117

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allfields	10.1186/BF03352100 doi (DE-627)SPR036894117 (SPR)BF03352100-e DE-627 ger DE-627 rakwb eng 550 VZ 38.70 bkl 39.22 bkl Yamamoto, T. verfasserin aut The PLANET-B mission 1998 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Society of Geomagnetism and Earth, Planetary and Space Sciences (SGEPSS); The Seismological Society of Japan; The Volcanological Society of Japan; The Geodetic Society of Japan; The Japanese Society for Planetary Sciences. 1998 Abstract PLANET-B is the Japanese Mars orbiter program. The spacecraft will begin its journey to Mars in July 1998, and will be inserted into Mars orbit in October 1999. It will collect data for at least one Martian year (about two Earth years). The primary objective of the program is to study the Martian aeronomy, with emphasis on the interaction of the Martian upper atmosphere with the solar wind. The periapsis altitude and the apoapsis distance are 150 km and 15 Mars radii, respectively. The dry weight of the orbiter is 258 kg including 15 scientific instruments. Advanced technologies are employed in the design of the spacecraft in attempt to overcome the mass limitation. This paper describes the scientific objectives of the PLANET-B program and the outline of the observation scenario. Solar Wind (dpeaa)DE-He213 Solar Zenith Angle (dpeaa)DE-He213 Parking Orbit (dpeaa)DE-He213 Mars Orbit (dpeaa)DE-He213 Martian Ionosphere (dpeaa)DE-He213 Tsuruda, K. verfasserin aut Enthalten in Earth, planets and space Springer Berlin Heidelberg, 1998 50(1998), 3 vom: März, Seite 175-181 (DE-627)353898597 (DE-600)2087663-4 1880-5981 nnns volume:50 year:1998 number:3 month:03 pages:175-181 https://dx.doi.org/10.1186/BF03352100 X:SPRINGER Resolving-System lizenzpflichtig Volltext SYSFLAG_0 GBV_SPRINGER SSG-OPC-GGO SSG-OPC-GEO SSG-OPC-AST GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 38.70 VZ 39.22 VZ AR 50 1998 3 03 175-181
spelling	10.1186/BF03352100 doi (DE-627)SPR036894117 (SPR)BF03352100-e DE-627 ger DE-627 rakwb eng 550 VZ 38.70 bkl 39.22 bkl Yamamoto, T. verfasserin aut The PLANET-B mission 1998 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Society of Geomagnetism and Earth, Planetary and Space Sciences (SGEPSS); The Seismological Society of Japan; The Volcanological Society of Japan; The Geodetic Society of Japan; The Japanese Society for Planetary Sciences. 1998 Abstract PLANET-B is the Japanese Mars orbiter program. The spacecraft will begin its journey to Mars in July 1998, and will be inserted into Mars orbit in October 1999. It will collect data for at least one Martian year (about two Earth years). The primary objective of the program is to study the Martian aeronomy, with emphasis on the interaction of the Martian upper atmosphere with the solar wind. The periapsis altitude and the apoapsis distance are 150 km and 15 Mars radii, respectively. The dry weight of the orbiter is 258 kg including 15 scientific instruments. Advanced technologies are employed in the design of the spacecraft in attempt to overcome the mass limitation. This paper describes the scientific objectives of the PLANET-B program and the outline of the observation scenario. Solar Wind (dpeaa)DE-He213 Solar Zenith Angle (dpeaa)DE-He213 Parking Orbit (dpeaa)DE-He213 Mars Orbit (dpeaa)DE-He213 Martian Ionosphere (dpeaa)DE-He213 Tsuruda, K. verfasserin aut Enthalten in Earth, planets and space Springer Berlin Heidelberg, 1998 50(1998), 3 vom: März, Seite 175-181 (DE-627)353898597 (DE-600)2087663-4 1880-5981 nnns volume:50 year:1998 number:3 month:03 pages:175-181 https://dx.doi.org/10.1186/BF03352100 X:SPRINGER Resolving-System lizenzpflichtig Volltext SYSFLAG_0 GBV_SPRINGER SSG-OPC-GGO SSG-OPC-GEO SSG-OPC-AST GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 38.70 VZ 39.22 VZ AR 50 1998 3 03 175-181
allfields_unstemmed	10.1186/BF03352100 doi (DE-627)SPR036894117 (SPR)BF03352100-e DE-627 ger DE-627 rakwb eng 550 VZ 38.70 bkl 39.22 bkl Yamamoto, T. verfasserin aut The PLANET-B mission 1998 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Society of Geomagnetism and Earth, Planetary and Space Sciences (SGEPSS); The Seismological Society of Japan; The Volcanological Society of Japan; The Geodetic Society of Japan; The Japanese Society for Planetary Sciences. 1998 Abstract PLANET-B is the Japanese Mars orbiter program. The spacecraft will begin its journey to Mars in July 1998, and will be inserted into Mars orbit in October 1999. It will collect data for at least one Martian year (about two Earth years). The primary objective of the program is to study the Martian aeronomy, with emphasis on the interaction of the Martian upper atmosphere with the solar wind. The periapsis altitude and the apoapsis distance are 150 km and 15 Mars radii, respectively. The dry weight of the orbiter is 258 kg including 15 scientific instruments. Advanced technologies are employed in the design of the spacecraft in attempt to overcome the mass limitation. This paper describes the scientific objectives of the PLANET-B program and the outline of the observation scenario. Solar Wind (dpeaa)DE-He213 Solar Zenith Angle (dpeaa)DE-He213 Parking Orbit (dpeaa)DE-He213 Mars Orbit (dpeaa)DE-He213 Martian Ionosphere (dpeaa)DE-He213 Tsuruda, K. verfasserin aut Enthalten in Earth, planets and space Springer Berlin Heidelberg, 1998 50(1998), 3 vom: März, Seite 175-181 (DE-627)353898597 (DE-600)2087663-4 1880-5981 nnns volume:50 year:1998 number:3 month:03 pages:175-181 https://dx.doi.org/10.1186/BF03352100 X:SPRINGER Resolving-System lizenzpflichtig Volltext SYSFLAG_0 GBV_SPRINGER SSG-OPC-GGO SSG-OPC-GEO SSG-OPC-AST GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 38.70 VZ 39.22 VZ AR 50 1998 3 03 175-181
allfieldsGer	10.1186/BF03352100 doi (DE-627)SPR036894117 (SPR)BF03352100-e DE-627 ger DE-627 rakwb eng 550 VZ 38.70 bkl 39.22 bkl Yamamoto, T. verfasserin aut The PLANET-B mission 1998 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Society of Geomagnetism and Earth, Planetary and Space Sciences (SGEPSS); The Seismological Society of Japan; The Volcanological Society of Japan; The Geodetic Society of Japan; The Japanese Society for Planetary Sciences. 1998 Abstract PLANET-B is the Japanese Mars orbiter program. The spacecraft will begin its journey to Mars in July 1998, and will be inserted into Mars orbit in October 1999. It will collect data for at least one Martian year (about two Earth years). The primary objective of the program is to study the Martian aeronomy, with emphasis on the interaction of the Martian upper atmosphere with the solar wind. The periapsis altitude and the apoapsis distance are 150 km and 15 Mars radii, respectively. The dry weight of the orbiter is 258 kg including 15 scientific instruments. Advanced technologies are employed in the design of the spacecraft in attempt to overcome the mass limitation. This paper describes the scientific objectives of the PLANET-B program and the outline of the observation scenario. Solar Wind (dpeaa)DE-He213 Solar Zenith Angle (dpeaa)DE-He213 Parking Orbit (dpeaa)DE-He213 Mars Orbit (dpeaa)DE-He213 Martian Ionosphere (dpeaa)DE-He213 Tsuruda, K. verfasserin aut Enthalten in Earth, planets and space Springer Berlin Heidelberg, 1998 50(1998), 3 vom: März, Seite 175-181 (DE-627)353898597 (DE-600)2087663-4 1880-5981 nnns volume:50 year:1998 number:3 month:03 pages:175-181 https://dx.doi.org/10.1186/BF03352100 X:SPRINGER Resolving-System lizenzpflichtig Volltext SYSFLAG_0 GBV_SPRINGER SSG-OPC-GGO SSG-OPC-GEO SSG-OPC-AST GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 38.70 VZ 39.22 VZ AR 50 1998 3 03 175-181
allfieldsSound	10.1186/BF03352100 doi (DE-627)SPR036894117 (SPR)BF03352100-e DE-627 ger DE-627 rakwb eng 550 VZ 38.70 bkl 39.22 bkl Yamamoto, T. verfasserin aut The PLANET-B mission 1998 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Society of Geomagnetism and Earth, Planetary and Space Sciences (SGEPSS); The Seismological Society of Japan; The Volcanological Society of Japan; The Geodetic Society of Japan; The Japanese Society for Planetary Sciences. 1998 Abstract PLANET-B is the Japanese Mars orbiter program. The spacecraft will begin its journey to Mars in July 1998, and will be inserted into Mars orbit in October 1999. It will collect data for at least one Martian year (about two Earth years). The primary objective of the program is to study the Martian aeronomy, with emphasis on the interaction of the Martian upper atmosphere with the solar wind. The periapsis altitude and the apoapsis distance are 150 km and 15 Mars radii, respectively. The dry weight of the orbiter is 258 kg including 15 scientific instruments. Advanced technologies are employed in the design of the spacecraft in attempt to overcome the mass limitation. This paper describes the scientific objectives of the PLANET-B program and the outline of the observation scenario. Solar Wind (dpeaa)DE-He213 Solar Zenith Angle (dpeaa)DE-He213 Parking Orbit (dpeaa)DE-He213 Mars Orbit (dpeaa)DE-He213 Martian Ionosphere (dpeaa)DE-He213 Tsuruda, K. verfasserin aut Enthalten in Earth, planets and space Springer Berlin Heidelberg, 1998 50(1998), 3 vom: März, Seite 175-181 (DE-627)353898597 (DE-600)2087663-4 1880-5981 nnns volume:50 year:1998 number:3 month:03 pages:175-181 https://dx.doi.org/10.1186/BF03352100 X:SPRINGER Resolving-System lizenzpflichtig Volltext SYSFLAG_0 GBV_SPRINGER SSG-OPC-GGO SSG-OPC-GEO SSG-OPC-AST GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 38.70 VZ 39.22 VZ AR 50 1998 3 03 175-181
language	English
source	Enthalten in Earth, planets and space 50(1998), 3 vom: März, Seite 175-181 volume:50 year:1998 number:3 month:03 pages:175-181
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institution	findex.gbv.de
topic_facet	Solar Wind Solar Zenith Angle Parking Orbit Mars Orbit Martian Ionosphere
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container_title	Earth, planets and space
authorswithroles_txt_mv	Yamamoto, T. @@aut@@ Tsuruda, K. @@aut@@
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author	Yamamoto, T.
spellingShingle	Yamamoto, T. ddc 550 bkl 38.70 bkl 39.22 misc Solar Wind misc Solar Zenith Angle misc Parking Orbit misc Mars Orbit misc Martian Ionosphere The PLANET-B mission
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title_auth	The PLANET-B mission
abstract	Abstract PLANET-B is the Japanese Mars orbiter program. The spacecraft will begin its journey to Mars in July 1998, and will be inserted into Mars orbit in October 1999. It will collect data for at least one Martian year (about two Earth years). The primary objective of the program is to study the Martian aeronomy, with emphasis on the interaction of the Martian upper atmosphere with the solar wind. The periapsis altitude and the apoapsis distance are 150 km and 15 Mars radii, respectively. The dry weight of the orbiter is 258 kg including 15 scientific instruments. Advanced technologies are employed in the design of the spacecraft in attempt to overcome the mass limitation. This paper describes the scientific objectives of the PLANET-B program and the outline of the observation scenario. © The Society of Geomagnetism and Earth, Planetary and Space Sciences (SGEPSS); The Seismological Society of Japan; The Volcanological Society of Japan; The Geodetic Society of Japan; The Japanese Society for Planetary Sciences. 1998
abstractGer	Abstract PLANET-B is the Japanese Mars orbiter program. The spacecraft will begin its journey to Mars in July 1998, and will be inserted into Mars orbit in October 1999. It will collect data for at least one Martian year (about two Earth years). The primary objective of the program is to study the Martian aeronomy, with emphasis on the interaction of the Martian upper atmosphere with the solar wind. The periapsis altitude and the apoapsis distance are 150 km and 15 Mars radii, respectively. The dry weight of the orbiter is 258 kg including 15 scientific instruments. Advanced technologies are employed in the design of the spacecraft in attempt to overcome the mass limitation. This paper describes the scientific objectives of the PLANET-B program and the outline of the observation scenario. © The Society of Geomagnetism and Earth, Planetary and Space Sciences (SGEPSS); The Seismological Society of Japan; The Volcanological Society of Japan; The Geodetic Society of Japan; The Japanese Society for Planetary Sciences. 1998
abstract_unstemmed	Abstract PLANET-B is the Japanese Mars orbiter program. The spacecraft will begin its journey to Mars in July 1998, and will be inserted into Mars orbit in October 1999. It will collect data for at least one Martian year (about two Earth years). The primary objective of the program is to study the Martian aeronomy, with emphasis on the interaction of the Martian upper atmosphere with the solar wind. The periapsis altitude and the apoapsis distance are 150 km and 15 Mars radii, respectively. The dry weight of the orbiter is 258 kg including 15 scientific instruments. Advanced technologies are employed in the design of the spacecraft in attempt to overcome the mass limitation. This paper describes the scientific objectives of the PLANET-B program and the outline of the observation scenario. © The Society of Geomagnetism and Earth, Planetary and Space Sciences (SGEPSS); The Seismological Society of Japan; The Volcanological Society of Japan; The Geodetic Society of Japan; The Japanese Society for Planetary Sciences. 1998
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title_short	The PLANET-B mission
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