Nanosat 01 (original) (raw)
El Nanosat 01 fue un satélite artificial español desarrollado por el Instituto Nacional de Técnica Aeroespacial y lanzado el 18 de diciembre de 2004.
| Property | Value |
|---|---|
| dbo:SpaceMission/missionDuration | 1461.0 (dbd:day) |
| dbo:abstract | El Nanosat 01 va ser un satèl·lit artificial desenvolupat per l'Institut Nacional de Tècnica Aeroespacial d'Espanya i llançat el 18 de desembre de 2004. El satèl·lit pesava menys de 20 kg, entrant en la categoria dels nanosatèl·lits i va ser llançat com a càrrega de pagament en un coet Ariane 5 des del Port Espacial Europeu de Kourou, al costat dels satèl·lits Helis 2A, Essaim 1, Essaim 2, Essaim 3, Essaim 4 i PARASOL. El Nanosat tenia forma de prisma de base hexagonal i estava totalment cobert de panells solars. Comptava amb quatre experiments, dos d'ells científics. Un altre dels objectius era servir d'enllaç amb la Base Antàrtica Joan Carles I. Posteriorment seria llançat el seu successor, el Nanosat-1B, en 2009, atès que la vida útil del primer era a punt d'expirar. (ca) El Nanosat 01 fue un satélite artificial español desarrollado por el Instituto Nacional de Técnica Aeroespacial y lanzado el 18 de diciembre de 2004. (es) The Nanosat 01, sometimes written as NanoSat-1 or NanoSat 01, was an artificial satellite developed by the Spanish Instituto Nacional de Técnica Aeroespacial (INTA) and launched the 18th of December 2004. Considered a nano satellite for its weight of less than 20 kg, its main mission was forwarding communications between far reaching points of the Earth such as Juan Carlos I Antarctic Base from mainland Spain. This was possible due to its polar orbit and altitude of 650 km above sea level. During an operational run the data obtained in the Antarctic would be uploaded to the satellite during its fly by and then, downloaded in Spain when satellite reached the Iberian Peninsula. When its service life came to an end in 2009, it was replaced by the Nanosat-1B, also developed by INTA. (en) Nanosat 01 était un satellite artificiel développé par l'Institut national de technique aérospatiale et lancé le 18 décembre 2004. Le satellite pesait moins de 20 kg, entrant dans la catégorie des nanosatellites et a été lancé par une fusée Ariane 5 depuis le Centre spatial guyanais, aux côtés des satellites Helios 2A, Essaim 1, 2, 3, 4 et PARASOL. (fr) |
| dbo:launchDate | 2004-12-18 (xsd:date) |
| dbo:launchVehicle | dbr:Ariane_5 |
| dbo:manufacturer | dbr:European_Space_Agency dbr:Spanish_National_Research_Council dbr:Instituto_Nacional_de_Técnica_Aeroespacial |
| dbo:missionDuration | 126230400.000000 (xsd:double) |
| dbo:operator | dbr:Instituto_Nacional_de_Técnica_Aeroespacial |
| dbo:thumbnail | wiki-commons:Special:FilePath/Nanosat_01,_INTA,_Madrid,_2015.jpg?width=300 |
| dbo:wikiPageExternalLink | http://www.inta.es/ http://space.skyrocket.de/doc_sdat/nanosat-01.htm |
| dbo:wikiPageID | 63610445 (xsd:integer) |
| dbo:wikiPageLength | 20338 (xsd:nonNegativeInteger) |
| dbo:wikiPageRevisionID | 1110528004 (xsd:integer) |
| dbo:wikiPageWikiLink | dbr:Ampere_hour dbr:Amplitude-shift_keying dbr:Programmable_read-only_memory dbr:Electrical_wiring dbr:Modulation dbr:Nanoparticle dbr:Apsis dbr:Honeywell dbr:Juan_Carlos_I_Antarctic_Base dbr:Lithium-ion_battery dbr:Revolutions_per_minute dbr:Ultra_high_frequency dbr:Infrared dbr:Input/output dbr:Nanotechnology dbr:Peninsular_Spain dbr:Essaim_(satellite) dbr:Omnidirectional_antenna dbr:Transparency_and_translucency dbr:Electric_motor dbr:Frequency-division_multiple_access dbr:Antarctic dbc:Spacecraft_launched_by_Ariane_rockets dbr:Light-emitting_diode dbr:Silicon_dioxide dbr:Closed-loop_communication dbr:Commercial_off-the-shelf dbr:Communications_satellite dbr:Compass dbr:Rotation_around_a_fixed_axis dbr:Orbital_period dbr:Photodiode dbr:Store_and_forward dbr:Stream_processing dbr:Torrejón_de_Ardoz dbr:Watt dbr:Helios_2_(satellite) dbr:Miniaturization dbr:DSP_Group dbr:EEPROM dbr:Earth dbr:Earth's_magnetic_field dbc:Satellites_of_Spain dbr:European_Space_Agency dbr:Faraday_effect dbr:Bandwidth_(computing) dbr:Parasol_(satellite) dbr:Digital_AMPS dbr:Direction_générale_de_l'armement dbr:Kilobyte dbr:Technology_demonstration dbr:Prism_(optics) dbr:Radar_cross-section dbr:Radio_frequency dbr:Resolution_(electron_density) dbr:Guiana_Space_Centre dbr:Hertz dbr:Hexagon dbr:Attitude_control dbr:Ionizing_radiation dbr:Iron(III)_oxide dbr:Tesla_(unit) dbr:Polarimetry dbr:Ariane_5 dbr:ALOHAnet dbc:Communications_satellites_in_low_Earth_orbit dbc:Spacecraft_launched_in_2004 dbr:Aerospace_manufacturer dbr:Sun dbr:Sun-synchronous_orbit dbr:Trapezoid dbr:Austenite dbr:Solar_cell dbr:Solar_panel dbr:Spanish_National_Research_Council dbr:Filter_(signal_processing) dbr:Freescale_DragonBall dbr:Frequency-shift_keying dbr:Iberian_Peninsula dbr:Instituto_Nacional_de_Técnica_Aeroespacial dbr:Nanosat-1B dbr:Nutation dbr:Random-access_memory dbr:Semi-major_and_semi-minor_axes dbr:Sensor dbr:Serial_Peripheral_Interface dbr:Printed_circuit_board dbr:Orbital_inclination dbr:Magnetism dbr:Magnetometer dbr:Megabyte dbr:Satellite dbr:Sensitivity_(electronics) dbr:Wavelength dbr:Polar_orbit dbr:Polarizer dbr:Viterbi_decoder dbr:Superparamagnetism dbr:Photodetector dbr:Verdet_constant dbr:Small_satellite dbr:Orbital_plane_(astronomy) dbr:Ascending_node dbr:Voltage/frequency_converter dbr:Wavelength-division_multiple_access dbr:File:Faraday-effect.png dbr:File:Photodiode-closeup.jpg |
| dbp:date | December 2020 (en) |
| dbp:dryMass | 19.0 (dbd:kilogram) |
| dbp:imageCaption | Replica of the Nanosat 01 at Homsec, Madrid (en) |
| dbp:insignia | Insignia Nanosat 01.png (en) |
| dbp:launchDate | 2004-12-18 (xsd:date) |
| dbp:launchRocket | dbr:Ariane_5 |
| dbp:launchSite | dbr:Guiana_Space_Centre |
| dbp:manufacturer | INTA, ESA, CSIC (en) |
| dbp:missionDuration | 1.262304E8 (dbd:second) |
| dbp:name | Nanosat 01 (en) |
| dbp:operator | dbr:Instituto_Nacional_de_Técnica_Aeroespacial |
| dbp:orbitAltitude | 656.5 (dbd:kilometre) |
| dbp:orbitApoapsis | 658.7 (dbd:kilometre) |
| dbp:orbitInclination | 98.100000 (xsd:double) |
| dbp:orbitPeriapsis | 654.2 (dbd:kilometre) |
| dbp:orbitPeriod | 5862.0 (dbd:second) |
| dbp:payloadItems | ACS, Earth magnetic nanosensor, Solar sensors, OWLS (en) |
| dbp:power | 17.0 (dbd:watt) |
| dbp:reason | unclear (en) |
| dbp:wikiPageUsesTemplate | dbt:Citation_needed dbt:Clarify dbt:Commons_category dbt:In_lang dbt:Portal_bar dbt:Spacecraft dbt:Orbital_launches_in_2004 dbt:Space_program_of_Spain |
| dct:subject | dbc:Spacecraft_launched_by_Ariane_rockets dbc:Satellites_of_Spain dbc:Communications_satellites_in_low_Earth_orbit dbc:Spacecraft_launched_in_2004 |
| rdf:type | owl:Thing schema:Event dul:Event dbo:SocietalEvent wikidata:Q1656682 wikidata:Q2133344 dbo:Event dbo:SpaceMission |
| rdfs:comment | El Nanosat 01 fue un satélite artificial español desarrollado por el Instituto Nacional de Técnica Aeroespacial y lanzado el 18 de diciembre de 2004. (es) Nanosat 01 était un satellite artificiel développé par l'Institut national de technique aérospatiale et lancé le 18 décembre 2004. Le satellite pesait moins de 20 kg, entrant dans la catégorie des nanosatellites et a été lancé par une fusée Ariane 5 depuis le Centre spatial guyanais, aux côtés des satellites Helios 2A, Essaim 1, 2, 3, 4 et PARASOL. (fr) El Nanosat 01 va ser un satèl·lit artificial desenvolupat per l'Institut Nacional de Tècnica Aeroespacial d'Espanya i llançat el 18 de desembre de 2004. El satèl·lit pesava menys de 20 kg, entrant en la categoria dels nanosatèl·lits i va ser llançat com a càrrega de pagament en un coet Ariane 5 des del Port Espacial Europeu de Kourou, al costat dels satèl·lits Helis 2A, Essaim 1, Essaim 2, Essaim 3, Essaim 4 i PARASOL. El Nanosat tenia forma de prisma de base hexagonal i estava totalment cobert de panells solars. Comptava amb quatre experiments, dos d'ells científics. Un altre dels objectius era servir d'enllaç amb la Base Antàrtica Joan Carles I. (ca) The Nanosat 01, sometimes written as NanoSat-1 or NanoSat 01, was an artificial satellite developed by the Spanish Instituto Nacional de Técnica Aeroespacial (INTA) and launched the 18th of December 2004. Considered a nano satellite for its weight of less than 20 kg, its main mission was forwarding communications between far reaching points of the Earth such as Juan Carlos I Antarctic Base from mainland Spain. This was possible due to its polar orbit and altitude of 650 km above sea level. During an operational run the data obtained in the Antarctic would be uploaded to the satellite during its fly by and then, downloaded in Spain when satellite reached the Iberian Peninsula. (en) |
| rdfs:label | Nanosat 01 (ca) Nanosat 01 (es) Nanosat 01 (fr) Nanosat 01 (en) |
| owl:sameAs | wikidata:Nanosat 01 dbpedia-ca:Nanosat 01 dbpedia-es:Nanosat 01 dbpedia-fr:Nanosat 01 dbpedia-gl:Nanosat 01 dbpedia-hu:Nanosat 01 https://global.dbpedia.org/id/4nK7X |
| prov:wasDerivedFrom | wikipedia-en:Nanosat_01?oldid=1110528004&ns=0 |
| foaf:depiction | wiki-commons:Special:FilePath/Faraday-effect.png wiki-commons:Special:FilePath/Insignia_Nanosat_01.png wiki-commons:Special:FilePath/Photodiode-closeup.jpg wiki-commons:Special:FilePath/Nanosat_01,_INTA,_Madrid,_2015.jpg |
| foaf:homepage | http://www.inta.es/ |
| foaf:isPrimaryTopicOf | wikipedia-en:Nanosat_01 |
| foaf:name | Nanosat 01 (en) |
| is dbo:wikiPageWikiLink of | dbr:Capricornio_(rocket) dbr:OPTOS dbr:2004_in_spaceflight dbr:List_of_Ariane_launches_(2000–2009) dbr:ELA-3 dbr:Ariane_5 dbr:INTA-100 dbr:Instituto_Nacional_de_Técnica_Aeroespacial dbr:Nanosat-1B |
| is foaf:primaryTopic of | wikipedia-en:Nanosat_01 |
