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Statements

Subject Item
dbr:Long_March_1D
rdf:type
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rdfs:label
Lunga Marcia 1D Longa Marcha 1D 長征一號丁運載火箭 창정 1D Чанчжэн-1D Long March 1D Long March 1D Dlouhý pochod 1D
rdfs:comment
창정 1D(중국어: 长征一号丁, 영어: Long March 1D, CZ-1D)는 창정 발사체 중 하나로, 창정 1 및 DF-4의 개량형으로서, 창정 1의 특성을 많이 갖고 있다. 창정 1D는 작은 페이로드를 우주 궤도로 쏘아올리기 위해 개발되었고, 1997년 11월 1일 최초 발사를 성공적으로 마쳤으며, 총 3번 발사되어 2번 성공하고 1번 실패했지만 위성 발사는 한 번도 해보지 못하였으며, 현재는 은퇴한 상태이다. 1990년대 말 중국운재화전기술연구원은 DF-31의 대기권 재진입 실험을 위해 DF-4의 개량형 개발에 착수하고, 후에 이 개량형 로켓이 창정 1D가 되었다. 그 후, 로켓은 작은 발사체로서 발사체 시장에 내놓아졌다. 长征一号丁运载火箭（缩写：CZ-1D 或 LM-1D）是长征一号的改进型，三次試射，两成一败，现已退役。主要的改进有：一子级发动机推力由1020千牛提高到1101.2千牛，提高了二、三两个子级性能。经改进后的长征一号D火箭能发射各种低轨道卫星，卫星入轨姿态既可以是自旋、也可以是三轴稳定状态。 Dlouhý pochod 1D je vylepšená verze rakety DP - 1. * nové motory prvního stupně YF-2B (dva paralelní YF-1B) * nové motory druhého stupně dva YF-40 * nový motor třetího stupně FG-36 * mezistupeň má nyní tvar válce protože třetí stupeň má nyní 2,05 m místo 1,5 m * lepší řídící počítač Longa Marcha 1D (长征一号), ou Changzheng-1 (CZ-1D), foi o segundo membro da família de foguetes chineses Longa Marcha, era uma evolução do Longa Marcha 1. O primeiro voo do modelo Longa Marcha 1D, ocorreu em Maio de 1995. Era um foguete de 3 estágios, sendo os dois primeiros movidos a combustível líquido e o terceiro, movido a combustível sólido. Ele efetuou apenas três voos até 3 de Janeiro de 2002 quando foi abandonado. Durante gli anni 90 l' ha sviluppato una versione migliorata del missile DF-4 allo scopo di testare un veicolo per il rientro atmosferico. A questo nuovo lanciatore venne dato il nome commerciale di Lunga Marcia 1D (in cinese: 长征一号丁S, Chángzhēng yīhào dīngP). Il Lunga Marcia 1D non ottenne un alto gradimento e venne utilizzato solo per test di rientro. Ha effettuato in totale tre voli suborbitali dal Cosmodromo di Taiyuan, di cui due completati con successo e uno, l'ultimo, concluso con un fallimento. Long March 1D adalah versi perbaikan dari roket Long March tahap 1 untuk kerajinan badan antariksa China, terutama untuk thrustor tahap 1, dari 1.020 kilonewtons ke 1101,2 kilonewtons, juga meningkatkan kinerja untuk tahap 2 dan tahap 3. Peningkatan Long March 1D bisa meluncurkan varian satelit LEO, orientasi satelit dapat berputar atau non-rotating. Penerbangan pertama pada bulan November 1997 berhasil. The Long March 1D was a member of China's Long March rocket family. During the 1990s CALT developed an improved version of the DF-4 to test the reentry vehicle warheads of the DF-31. They took advantage of this development and offered it as the Long March 1D for commercial application. The modifications included: Чанчжэн 1D, или CZ-1D, или LM-1D (кит. трад. 長征一號D, упр. 长征一号D, пиньинь Chángzhēng yī hào D, палл. Чанчжэн и хао D , буквально Чанчжэн 1D) — китайская трёхступенчатая ракета-носитель лёгкого класса, семейства «Чанчжэн».
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1995-06-01
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dbo:abstract
Long March 1D adalah versi perbaikan dari roket Long March tahap 1 untuk kerajinan badan antariksa China, terutama untuk thrustor tahap 1, dari 1.020 kilonewtons ke 1101,2 kilonewtons, juga meningkatkan kinerja untuk tahap 2 dan tahap 3. Peningkatan Long March 1D bisa meluncurkan varian satelit LEO, orientasi satelit dapat berputar atau non-rotating. Penerbangan pertama pada bulan November 1997 berhasil. Longa Marcha 1D (长征一号), ou Changzheng-1 (CZ-1D), foi o segundo membro da família de foguetes chineses Longa Marcha, era uma evolução do Longa Marcha 1. O primeiro voo do modelo Longa Marcha 1D, ocorreu em Maio de 1995. Era um foguete de 3 estágios, sendo os dois primeiros movidos a combustível líquido e o terceiro, movido a combustível sólido. Ele efetuou apenas três voos até 3 de Janeiro de 2002 quando foi abandonado. Esse modelo, era um pouco menor que seu antecessor, mas usava um segundo estágio mais moderno e eficiente. Seu objetivo primário, era efetuar testes de veículos de reentrada suborbital, e nunca chegou a efetuar um voo orbital. The Long March 1D was a member of China's Long March rocket family. During the 1990s CALT developed an improved version of the DF-4 to test the reentry vehicle warheads of the DF-31. They took advantage of this development and offered it as the Long March 1D for commercial application. The modifications included: * An DF-4 improved first stage, which used the new version of the YF-2B, and switched propellants to UDMH/N2O4 for improved performance. * The replacement of the DF-4 second stage motor YF-3A. The proposed replacement was the Long March 4 third stage engine, the YF-40. * A new inline inter-stage would replace the existing tapered connector between the second and third stages, which allowed for an additional 70cm diameter to be added to the third stage skirt. This would allow for the addition of RCS to the third stage. * A new third stage with a new motor, the FG-36 and an optional RCS. * A new computer inertial guidance system which enabled the third stage to be 3-axis stabilised for added precision. The new design did not have a good reception and was only used for reentry vehicle tests. It flew three suborbital missions from Taiyuan LC-1 with two successes and a failure on the final mission. The first launch was on June 1, 1995 and the second one was in November 1997. The final and failed launch was on January 3, 2002. 长征一号丁运载火箭（缩写：CZ-1D 或 LM-1D）是长征一号的改进型，三次試射，两成一败，现已退役。主要的改进有：一子级发动机推力由1020千牛提高到1101.2千牛，提高了二、三两个子级性能。经改进后的长征一号D火箭能发射各种低轨道卫星，卫星入轨姿态既可以是自旋、也可以是三轴稳定状态。 창정 1D(중국어: 长征一号丁, 영어: Long March 1D, CZ-1D)는 창정 발사체 중 하나로, 창정 1 및 DF-4의 개량형으로서, 창정 1의 특성을 많이 갖고 있다. 창정 1D는 작은 페이로드를 우주 궤도로 쏘아올리기 위해 개발되었고, 1997년 11월 1일 최초 발사를 성공적으로 마쳤으며, 총 3번 발사되어 2번 성공하고 1번 실패했지만 위성 발사는 한 번도 해보지 못하였으며, 현재는 은퇴한 상태이다. 1990년대 말 중국운재화전기술연구원은 DF-31의 대기권 재진입 실험을 위해 DF-4의 개량형 개발에 착수하고, 후에 이 개량형 로켓이 창정 1D가 되었다. 그 후, 로켓은 작은 발사체로서 발사체 시장에 내놓아졌다. Durante gli anni 90 l' ha sviluppato una versione migliorata del missile DF-4 allo scopo di testare un veicolo per il rientro atmosferico. A questo nuovo lanciatore venne dato il nome commerciale di Lunga Marcia 1D (in cinese: 长征一号丁S, Chángzhēng yīhào dīngP). Il Lunga Marcia 1D non ottenne un alto gradimento e venne utilizzato solo per test di rientro. Ha effettuato in totale tre voli suborbitali dal Cosmodromo di Taiyuan, di cui due completati con successo e uno, l'ultimo, concluso con un fallimento. Чанчжэн 1D, или CZ-1D, или LM-1D (кит. трад. 長征一號D, упр. 长征一号D, пиньинь Chángzhēng yī hào D, палл. Чанчжэн и хао D , буквально Чанчжэн 1D) — китайская трёхступенчатая ракета-носитель лёгкого класса, семейства «Чанчжэн». Dlouhý pochod 1D je vylepšená verze rakety DP - 1. * nové motory prvního stupně YF-2B (dva paralelní YF-1B) * nové motory druhého stupně dva YF-40 * nový motor třetího stupně FG-36 * mezistupeň má nyní tvar válce protože třetí stupeň má nyní 2,05 m místo 1,5 m * lepší řídící počítač
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