Long March 2C (original) (raw)
Dlouhý pochod 2C (CZ-2C, čínsky pchin-jinem Chángzhēng èrhàobǐng, znaky zjednodušené 长征二号丙, tradiční 長征二號丙) je čínská nosná raketa patřící do rodiny .
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| dbo:abstract | Dlouhý pochod 2C (CZ-2C, čínsky pchin-jinem Chángzhēng èrhàobǐng, znaky zjednodušené 长征二号丙, tradiční 長征二號丙) je čínská nosná raketa patřící do rodiny . (cs) Longue Marche 2C (CZ-2C) est un dérivé de la famille des fusées Longue Marche 2, un système de lancement durable géré par l'agence spatiale chinoise. Le premier lancement a eu lieu le 26 novembre 1975. Il s'agit d'une fusée a deux étages avec des propergols stockables, composés de tétroxyde d'azote et de diméthyle hydrazine asymétrique. Cette fusée est dérivée d'un missile balistique (DF-5) chinois. * Plusieurs variantes de ce véhicule de lancement ont été construites: * 2C/SD - lanceur de satellite commercial. * 2C/SD - lanceur permettant la livraison de deux satellites simultanément. * 2C/SM - Version améliorée. (fr) The Long March 2C (LM-2C), also known as the Chang Zheng 2C (CZ-2C), is a Chinese orbital launch vehicle, part of the Long March 2 rocket family. Developed and manufactured by the China Academy of Launch Vehicle Technology (CALT), the Long March 2C made its first launch on 9 September 1982. It is a two-stage launch vehicle with storable propellants, consisting of Nitrogen Tetroxide and Unsymmetrical Dimethylhydrazine. The launch vehicle was derived from the DF-5 ICBM. Several variants of this launch vehicle have been built, all using an optional third solid motor stage: * 2C/SD: Commercial satellite launcher with a multi-satellite smart dispenser allowing delivery of two satellites simultaneously * 2C/SM: Version for delivery of small satellites to high orbits * 2C/SMA: Improved version of the 2C/SM According to the website Gunter's Space Page, in addition to the launches listed in the following table, there may have been six additional CZ-2C launches during 2014 and 2015. These possible launches apparently were conducted at the Taiyuan Satellite Launch Center on the following dates: 9 January 2014, 7 August 2014, 2 December 2014, 7 June 2015, 20 August 2015, and 23 November 2015; five of these six launches were apparently successful, while the launch on 7 August 2014 appears to have failed. However, due to the lack of additional sources for these six launches, they are not currently included in the following launch list. Aerodynamic grid fins were added on the Long March 2C in 2019 to help guide falling stages away from populated areas. China is studying using reusable rocket technology in the future. A fairing recovery system through parachutes has been tested during the Yaogan 30-09 and Yaogan 30-10 launches in order to improve control of debris landing inland on potentially populated areas. (en) Long March 2C (LM-2C), atau Chang Zheng 2C (CZ-2C) seperti dalam bahasa Cina pinyin adalah anggota dari keluarga roket Long March 2, sebuah sistem peluncuran sekali pakai dioperasikan oleh Republik Rakyat Tiongkok. Kendaraan ini dikembangkan oleh China Academy of Launch Vehicle Technology, dan peluncuran pertama terjadi pada tanggal 26 November 1975. Roket ini adalah roket kendaraan peluncur dua tahap dengan propelan storable, terdiri dari Nitrogen Tetroxide dan Unsymmetrical Dimethyl Hydrazine. Mulai dari peluncuran pertamanya, Long March 2C memiliki 34 peluncuran sukses berturut-turut sampai kegagalan pertama pada tahun 2011. (in) Lunga Marcia 2C (in cinese: 長征二号丙S, Chángzhēng èrhào bǐngP) è un lanciatore spaziale cinese. È stato sviluppato dall' e il suo primo lancio è avvenuto il 9 settembre 1982. È un vettore a due stadi alimentato con tetraossido di diazoto e 1,1-dimetilidrazina ed è stato derivato dal Lunga Marcia 2A. Sono state prodotte numerose varianti del lanciatore, tutte con un terzo stadio opzionale a propellente solido: * 2C/SD — lanciatore spaziale commerciale in grado di trasportare due satelliti contemporaneamente * 2C/SM — versione per piccoli satelliti in orbite alte * 2C/SMA — versione migliorata del 2C/SM Il 18 agosto 2011 un vettore Lunga Marcia 2C che trasportava il satellite Shijian XI-01 fallì durante il lancio. Ciò avvenne a causa di un malfunzionamento del meccanismo di connessione tra il motore numero 3 e il servocontrollo del secondo stadio, il che portò ad una perdita del controllo dell'assetto del secondo stadio. (it) Chang Zheng 2C (chiń. 长征二号丙) – chińska rakieta nośna z rodziny rakiet Chang Zheng. Należy ona do rakiet o niskim udźwigu, więc może się równać z rakietami takimi jak europejska Vega czy Falcon 1 firmy SpaceX. CZ-2C jest wykorzystywana głównie do startów komercyjnych. (pl) Chang Zheng 2C (长征二号丙, CZ-2C) är en kinesisk rymdraket som flög för första gången 9 september 1982. (sv) Чанчжэн 2C или CZ-2C (кит. трад. 長征二號丙, упр. 长征二号丙, пиньинь Chángzhēng èr hào bǐng, палл. Чанчжэн эр хао бин, буквально Великий поход 2C) — двухступенчатая ракета-носитель Китайской Народной Республики серии «Чанчжэн». (ru) Longa Marcha 2C (LM-2C), ou Chang Zheng 2C (CZ-2C) é um foguete desenvolvido pela China. (pt) 长征二号丙运载火箭是在长征二号火箭的基础上改进设计的火箭，其近地轨道运载能力由原来的1800公斤提高到2500公斤，同时可靠性大大提高。發射一次的價格約為2500萬美元。長征二號丙運載火箭是中国航天运载火箭的基礎型號。在長征二號丙的技術基礎上，發展了長征三號系列運載火箭。 长征二号丙共有三種型號分支： * 长征二号丙/SD：1997年9月1日首次發射，是一種商業衛星發射器，即在长征二号丙的二級火箭上安裝一個上面級的智能分配器（Smart Dispenser），為並聯多星上面級。 * 长征二号丙/SM：2003年首次發射，上面級安裝了固体发动机（Solid Motor），用於發射高軌道衛星。 * 长征二号丙/SMA：2008年首次發射，安裝了改進版的智能分配器，為串聯多星上面級。 (zh) |
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| rdfs:comment | Dlouhý pochod 2C (CZ-2C, čínsky pchin-jinem Chángzhēng èrhàobǐng, znaky zjednodušené 长征二号丙, tradiční 長征二號丙) je čínská nosná raketa patřící do rodiny . (cs) Chang Zheng 2C (chiń. 长征二号丙) – chińska rakieta nośna z rodziny rakiet Chang Zheng. Należy ona do rakiet o niskim udźwigu, więc może się równać z rakietami takimi jak europejska Vega czy Falcon 1 firmy SpaceX. CZ-2C jest wykorzystywana głównie do startów komercyjnych. (pl) Chang Zheng 2C (长征二号丙, CZ-2C) är en kinesisk rymdraket som flög för första gången 9 september 1982. (sv) Чанчжэн 2C или CZ-2C (кит. трад. 長征二號丙, упр. 长征二号丙, пиньинь Chángzhēng èr hào bǐng, палл. Чанчжэн эр хао бин, буквально Великий поход 2C) — двухступенчатая ракета-носитель Китайской Народной Республики серии «Чанчжэн». (ru) Longa Marcha 2C (LM-2C), ou Chang Zheng 2C (CZ-2C) é um foguete desenvolvido pela China. (pt) 长征二号丙运载火箭是在长征二号火箭的基础上改进设计的火箭，其近地轨道运载能力由原来的1800公斤提高到2500公斤，同时可靠性大大提高。發射一次的價格約為2500萬美元。長征二號丙運載火箭是中国航天运载火箭的基礎型號。在長征二號丙的技術基礎上，發展了長征三號系列運載火箭。 长征二号丙共有三種型號分支： * 长征二号丙/SD：1997年9月1日首次發射，是一種商業衛星發射器，即在长征二号丙的二級火箭上安裝一個上面級的智能分配器（Smart Dispenser），為並聯多星上面級。 * 长征二号丙/SM：2003年首次發射，上面級安裝了固体发动机（Solid Motor），用於發射高軌道衛星。 * 长征二号丙/SMA：2008年首次發射，安裝了改進版的智能分配器，為串聯多星上面級。 (zh) The Long March 2C (LM-2C), also known as the Chang Zheng 2C (CZ-2C), is a Chinese orbital launch vehicle, part of the Long March 2 rocket family. Developed and manufactured by the China Academy of Launch Vehicle Technology (CALT), the Long March 2C made its first launch on 9 September 1982. It is a two-stage launch vehicle with storable propellants, consisting of Nitrogen Tetroxide and Unsymmetrical Dimethylhydrazine. The launch vehicle was derived from the DF-5 ICBM. Several variants of this launch vehicle have been built, all using an optional third solid motor stage: (en) Long March 2C (LM-2C), atau Chang Zheng 2C (CZ-2C) seperti dalam bahasa Cina pinyin adalah anggota dari keluarga roket Long March 2, sebuah sistem peluncuran sekali pakai dioperasikan oleh Republik Rakyat Tiongkok. Kendaraan ini dikembangkan oleh China Academy of Launch Vehicle Technology, dan peluncuran pertama terjadi pada tanggal 26 November 1975. (in) Longue Marche 2C (CZ-2C) est un dérivé de la famille des fusées Longue Marche 2, un système de lancement durable géré par l'agence spatiale chinoise. Le premier lancement a eu lieu le 26 novembre 1975. Il s'agit d'une fusée a deux étages avec des propergols stockables, composés de tétroxyde d'azote et de diméthyle hydrazine asymétrique. Cette fusée est dérivée d'un missile balistique (DF-5) chinois. (fr) Lunga Marcia 2C (in cinese: 長征二号丙S, Chángzhēng èrhào bǐngP) è un lanciatore spaziale cinese. È stato sviluppato dall' e il suo primo lancio è avvenuto il 9 settembre 1982. È un vettore a due stadi alimentato con tetraossido di diazoto e 1,1-dimetilidrazina ed è stato derivato dal Lunga Marcia 2A. Sono state prodotte numerose varianti del lanciatore, tutte con un terzo stadio opzionale a propellente solido: (it) |
| rdfs:label | Dlouhý pochod 2C (cs) Long March 2C (in) Longue Marche 2C (fr) Lunga Marcia 2C (it) Long March 2C (en) Chang Zheng 2C (pl) Longa Marcha 2C (pt) Чанчжэн-2C (ru) Chang Zheng 2C (sv) 长征二号丙运载火箭 (zh) |
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