. "\uCC3D\uC815 1D(\uC911\uAD6D\uC5B4: \u957F\u5F81\u4E00\u53F7\u4E01, \uC601\uC5B4: Long March 1D, CZ-1D)\uB294 \uCC3D\uC815 \uBC1C\uC0AC\uCCB4 \uC911 \uD558\uB098\uB85C, \uCC3D\uC815 1 \uBC0F DF-4\uC758 \uAC1C\uB7C9\uD615\uC73C\uB85C\uC11C, \uCC3D\uC815 1\uC758 \uD2B9\uC131\uC744 \uB9CE\uC774 \uAC16\uACE0 \uC788\uB2E4. \uCC3D\uC815 1D\uB294 \uC791\uC740 \uD398\uC774\uB85C\uB4DC\uB97C \uC6B0\uC8FC \uADA4\uB3C4\uB85C \uC3D8\uC544\uC62C\uB9AC\uAE30 \uC704\uD574 \uAC1C\uBC1C\uB418\uC5C8\uACE0, 1997\uB144 11\uC6D4 1\uC77C \uCD5C\uCD08 \uBC1C\uC0AC\uB97C \uC131\uACF5\uC801\uC73C\uB85C \uB9C8\uCCE4\uC73C\uBA70, \uCD1D 3\uBC88 \uBC1C\uC0AC\uB418\uC5B4 2\uBC88 \uC131\uACF5\uD558\uACE0 1\uBC88 \uC2E4\uD328\uD588\uC9C0\uB9CC \uC704\uC131 \uBC1C\uC0AC\uB294 \uD55C \uBC88\uB3C4 \uD574\uBCF4\uC9C0 \uBABB\uD558\uC600\uC73C\uBA70, \uD604\uC7AC\uB294 \uC740\uD1F4\uD55C \uC0C1\uD0DC\uC774\uB2E4. 1990\uB144\uB300 \uB9D0 \uC911\uAD6D\uC6B4\uC7AC\uD654\uC804\uAE30\uC220\uC5F0\uAD6C\uC6D0\uC740 DF-31\uC758 \uB300\uAE30\uAD8C \uC7AC\uC9C4\uC785 \uC2E4\uD5D8\uC744 \uC704\uD574 DF-4\uC758 \uAC1C\uB7C9\uD615 \uAC1C\uBC1C\uC5D0 \uCC29\uC218\uD558\uACE0, \uD6C4\uC5D0 \uC774 \uAC1C\uB7C9\uD615 \uB85C\uCF13\uC774 \uCC3D\uC815 1D\uAC00 \uB418\uC5C8\uB2E4. \uADF8 \uD6C4, \uB85C\uCF13\uC740 \uC791\uC740 \uBC1C\uC0AC\uCCB4\uB85C\uC11C \uBC1C\uC0AC\uCCB4 \uC2DC\uC7A5\uC5D0 \uB0B4\uB193\uC544\uC84C\uB2E4."@ko . "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."@in . . . "Longa Marcha 1D (\u957F\u5F81\u4E00\u53F7), ou Changzheng-1 (CZ-1D), foi o segundo membro da fam\u00EDlia de foguetes chineses Longa Marcha, era uma evolu\u00E7\u00E3o do Longa Marcha 1. O primeiro voo do modelo Longa Marcha 1D, ocorreu em Maio de 1995. Era um foguete de 3 est\u00E1gios, sendo os dois primeiros movidos a combust\u00EDvel l\u00EDquido e o terceiro, movido a combust\u00EDvel s\u00F3lido. Ele efetuou apenas tr\u00EAs voos at\u00E9 3 de Janeiro de 2002 quando foi abandonado. Esse modelo, era um pouco menor que seu antecessor, mas usava um segundo est\u00E1gio mais moderno e eficiente. Seu objetivo prim\u00E1rio, era efetuar testes de ve\u00EDculos de reentrada suborbital, e nunca chegou a efetuar um voo orbital."@pt . "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: \n* An DF-4 improved first stage, which used the new version of the YF-2B, and switched propellants to UDMH/N2O4 for improved performance. \n* 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. \n* 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. \n* A new third stage with a new motor, the FG-36 and an optional RCS. \n* 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."@en . "2"^^ . . "1995-06-01"^^ . "Lunga Marcia 1D"@it . . . . "China"@en . . "Longa Marcha 1D"@pt . "\u957F\u5F81\u4E00\u53F7\u4E01\u8FD0\u8F7D\u706B\u7BAD\uFF08\u7F29\u5199\uFF1ACZ-1D \u6216 LM-1D\uFF09\u662F\u957F\u5F81\u4E00\u53F7\u7684\u6539\u8FDB\u578B\uFF0C\u4E09\u6B21\u8A66\u5C04\uFF0C\u4E24\u6210\u4E00\u8D25\uFF0C\u73B0\u5DF2\u9000\u5F79\u3002\u4E3B\u8981\u7684\u6539\u8FDB\u6709\uFF1A\u4E00\u5B50\u7EA7\u53D1\u52A8\u673A\u63A8\u529B\u75311020\u5343\u725B\u63D0\u9AD8\u52301101.2\u5343\u725B\uFF0C\u63D0\u9AD8\u4E86\u4E8C\u3001\u4E09\u4E24\u4E2A\u5B50\u7EA7\u6027\u80FD\u3002\u7ECF\u6539\u8FDB\u540E\u7684\u957F\u5F81\u4E00\u53F7D\u706B\u7BAD\u80FD\u53D1\u5C04\u5404\u79CD\u4F4E\u8F68\u9053\u536B\u661F\uFF0C\u536B\u661F\u5165\u8F68\u59FF\u6001\u65E2\u53EF\u4EE5\u662F\u81EA\u65CB\u3001\u4E5F\u53EF\u4EE5\u662F\u4E09\u8F74\u7A33\u5B9A\u72B6\u6001\u3002"@zh . . "\u957F\u5F81\u4E00\u53F7\u4E01\u8FD0\u8F7D\u706B\u7BAD\uFF08\u7F29\u5199\uFF1ACZ-1D \u6216 LM-1D\uFF09\u662F\u957F\u5F81\u4E00\u53F7\u7684\u6539\u8FDB\u578B\uFF0C\u4E09\u6B21\u8A66\u5C04\uFF0C\u4E24\u6210\u4E00\u8D25\uFF0C\u73B0\u5DF2\u9000\u5F79\u3002\u4E3B\u8981\u7684\u6539\u8FDB\u6709\uFF1A\u4E00\u5B50\u7EA7\u53D1\u52A8\u673A\u63A8\u529B\u75311020\u5343\u725B\u63D0\u9AD8\u52301101.2\u5343\u725B\uFF0C\u63D0\u9AD8\u4E86\u4E8C\u3001\u4E09\u4E24\u4E2A\u5B50\u7EA7\u6027\u80FD\u3002\u7ECF\u6539\u8FDB\u540E\u7684\u957F\u5F81\u4E00\u53F7D\u706B\u7BAD\u80FD\u53D1\u5C04\u5404\u79CD\u4F4E\u8F68\u9053\u536B\u661F\uFF0C\u536B\u661F\u5165\u8F68\u59FF\u6001\u65E2\u53EF\u4EE5\u662F\u81EA\u65CB\u3001\u4E5F\u53EF\u4EE5\u662F\u4E09\u8F74\u7A33\u5B9A\u72B6\u6001\u3002"@zh . "2.25"^^ . . "Dlouh\u00FD pochod 1D je vylep\u0161en\u00E1 verze rakety DP - 1. \n* nov\u00E9 motory prvn\u00EDho stupn\u011B YF-2B (dva paraleln\u00ED YF-1B) \n* nov\u00E9 motory druh\u00E9ho stupn\u011B dva YF-40 \n* nov\u00FD motor t\u0159et\u00EDho stupn\u011B FG-36 \n* mezistupe\u0148 m\u00E1 nyn\u00ED tvar v\u00E1lce proto\u017Ee t\u0159et\u00ED stupe\u0148 m\u00E1 nyn\u00ED 2,05 m m\u00EDsto 1,5 m \n* lep\u0161\u00ED \u0159\u00EDd\u00EDc\u00ED po\u010D\u00EDta\u010D"@cs . . "81650.0"^^ . "Retired"@en . "Longa Marcha 1D (\u957F\u5F81\u4E00\u53F7), ou Changzheng-1 (CZ-1D), foi o segundo membro da fam\u00EDlia de foguetes chineses Longa Marcha, era uma evolu\u00E7\u00E3o do Longa Marcha 1. O primeiro voo do modelo Longa Marcha 1D, ocorreu em Maio de 1995. Era um foguete de 3 est\u00E1gios, sendo os dois primeiros movidos a combust\u00EDvel l\u00EDquido e o terceiro, movido a combust\u00EDvel s\u00F3lido. Ele efetuou apenas tr\u00EAs voos at\u00E9 3 de Janeiro de 2002 quando foi abandonado."@pt . "\uCC3D\uC815 1D(\uC911\uAD6D\uC5B4: \u957F\u5F81\u4E00\u53F7\u4E01, \uC601\uC5B4: Long March 1D, CZ-1D)\uB294 \uCC3D\uC815 \uBC1C\uC0AC\uCCB4 \uC911 \uD558\uB098\uB85C, \uCC3D\uC815 1 \uBC0F DF-4\uC758 \uAC1C\uB7C9\uD615\uC73C\uB85C\uC11C, \uCC3D\uC815 1\uC758 \uD2B9\uC131\uC744 \uB9CE\uC774 \uAC16\uACE0 \uC788\uB2E4. \uCC3D\uC815 1D\uB294 \uC791\uC740 \uD398\uC774\uB85C\uB4DC\uB97C \uC6B0\uC8FC \uADA4\uB3C4\uB85C \uC3D8\uC544\uC62C\uB9AC\uAE30 \uC704\uD574 \uAC1C\uBC1C\uB418\uC5C8\uACE0, 1997\uB144 11\uC6D4 1\uC77C \uCD5C\uCD08 \uBC1C\uC0AC\uB97C \uC131\uACF5\uC801\uC73C\uB85C \uB9C8\uCCE4\uC73C\uBA70, \uCD1D 3\uBC88 \uBC1C\uC0AC\uB418\uC5B4 2\uBC88 \uC131\uACF5\uD558\uACE0 1\uBC88 \uC2E4\uD328\uD588\uC9C0\uB9CC \uC704\uC131 \uBC1C\uC0AC\uB294 \uD55C \uBC88\uB3C4 \uD574\uBCF4\uC9C0 \uBABB\uD558\uC600\uC73C\uBA70, \uD604\uC7AC\uB294 \uC740\uD1F4\uD55C \uC0C1\uD0DC\uC774\uB2E4. 1990\uB144\uB300 \uB9D0 \uC911\uAD6D\uC6B4\uC7AC\uD654\uC804\uAE30\uC220\uC5F0\uAD6C\uC6D0\uC740 DF-31\uC758 \uB300\uAE30\uAD8C \uC7AC\uC9C4\uC785 \uC2E4\uD5D8\uC744 \uC704\uD574 DF-4\uC758 \uAC1C\uB7C9\uD615 \uAC1C\uBC1C\uC5D0 \uCC29\uC218\uD558\uACE0, \uD6C4\uC5D0 \uC774 \uAC1C\uB7C9\uD615 \uB85C\uCF13\uC774 \uCC3D\uC815 1D\uAC00 \uB418\uC5C8\uB2E4. \uADF8 \uD6C4, \uB85C\uCF13\uC740 \uC791\uC740 \uBC1C\uC0AC\uCCB4\uB85C\uC11C \uBC1C\uC0AC\uCCB4 \uC2DC\uC7A5\uC5D0 \uB0B4\uB193\uC544\uC84C\uB2E4."@ko . . . "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: \u957F\u5F81\u4E00\u53F7\u4E01S, Ch\u00E1ngzh\u0113ng y\u012Bh\u00E0o d\u012BngP). 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."@it . . . . "Long March 1D"@en . "2"^^ . . . . . "1084020865"^^ . . . . "2892589"^^ . "\u9577\u5F81\u4E00\u865F\u4E01\u904B\u8F09\u706B\u7BAD"@zh . . . . . . . . . . . "28.22"^^ . "\u0427\u0430\u043D\u0447\u0436\u044D\u043D 1D, \u0438\u043B\u0438 CZ-1D, \u0438\u043B\u0438 LM-1D (\u043A\u0438\u0442. \u0442\u0440\u0430\u0434. \u9577\u5F81\u4E00\u865FD, \u0443\u043F\u0440. \u957F\u5F81\u4E00\u53F7D, \u043F\u0438\u043D\u044C\u0438\u043D\u044C Ch\u00E1ngzh\u0113ng y\u012B h\u00E0o D, \u043F\u0430\u043B\u043B. \u0427\u0430\u043D\u0447\u0436\u044D\u043D \u0438 \u0445\u0430\u043E D , \u0431\u0443\u043A\u0432\u0430\u043B\u044C\u043D\u043E \u0427\u0430\u043D\u0447\u0436\u044D\u043D 1D) \u2014 \u043A\u0438\u0442\u0430\u0439\u0441\u043A\u0430\u044F \u0442\u0440\u0451\u0445\u0441\u0442\u0443\u043F\u0435\u043D\u0447\u0430\u0442\u0430\u044F \u0440\u0430\u043A\u0435\u0442\u0430-\u043D\u043E\u0441\u0438\u0442\u0435\u043B\u044C \u043B\u0451\u0433\u043A\u043E\u0433\u043E \u043A\u043B\u0430\u0441\u0441\u0430, \u0441\u0435\u043C\u0435\u0439\u0441\u0442\u0432\u0430 \u00AB\u0427\u0430\u043D\u0447\u0436\u044D\u043D\u00BB."@ru . . "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: \u957F\u5F81\u4E00\u53F7\u4E01S, Ch\u00E1ngzh\u0113ng y\u012Bh\u00E0o d\u012BngP). 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."@it . "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."@in . . . "3"^^ . . . . . "10936"^^ . "1995-06-01"^^ . . . "\uCC3D\uC815 1D"@ko . "3"^^ . . "1"^^ . . . "--03-01"^^ . . . . . . . . "\u0427\u0430\u043D\u0447\u0436\u044D\u043D-1D"@ru . "3"^^ . "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:"@en . . "2.25"^^ . "--03-01"^^ . . . . . . . "2002-01-03"^^ . . . "3"^^ . "Long March 1D"@en . "\u0427\u0430\u043D\u0447\u0436\u044D\u043D 1D, \u0438\u043B\u0438 CZ-1D, \u0438\u043B\u0438 LM-1D (\u043A\u0438\u0442. \u0442\u0440\u0430\u0434. \u9577\u5F81\u4E00\u865FD, \u0443\u043F\u0440. \u957F\u5F81\u4E00\u53F7D, \u043F\u0438\u043D\u044C\u0438\u043D\u044C Ch\u00E1ngzh\u0113ng y\u012B h\u00E0o D, \u043F\u0430\u043B\u043B. \u0427\u0430\u043D\u0447\u0436\u044D\u043D \u0438 \u0445\u0430\u043E D , \u0431\u0443\u043A\u0432\u0430\u043B\u044C\u043D\u043E \u0427\u0430\u043D\u0447\u0436\u044D\u043D 1D) \u2014 \u043A\u0438\u0442\u0430\u0439\u0441\u043A\u0430\u044F \u0442\u0440\u0451\u0445\u0441\u0442\u0443\u043F\u0435\u043D\u0447\u0430\u0442\u0430\u044F \u0440\u0430\u043A\u0435\u0442\u0430-\u043D\u043E\u0441\u0438\u0442\u0435\u043B\u044C \u043B\u0451\u0433\u043A\u043E\u0433\u043E \u043A\u043B\u0430\u0441\u0441\u0430, \u0441\u0435\u043C\u0435\u0439\u0441\u0442\u0432\u0430 \u00AB\u0427\u0430\u043D\u0447\u0436\u044D\u043D\u00BB."@ru . . . "2002-01-03"^^ . "Long March 1D"@in . "Dlouh\u00FD pochod 1D je vylep\u0161en\u00E1 verze rakety DP - 1. \n* nov\u00E9 motory prvn\u00EDho stupn\u011B YF-2B (dva paraleln\u00ED YF-1B) \n* nov\u00E9 motory druh\u00E9ho stupn\u011B dva YF-40 \n* nov\u00FD motor t\u0159et\u00EDho stupn\u011B FG-36 \n* mezistupe\u0148 m\u00E1 nyn\u00ED tvar v\u00E1lce proto\u017Ee t\u0159et\u00ED stupe\u0148 m\u00E1 nyn\u00ED 2,05 m m\u00EDsto 1,5 m \n* lep\u0161\u00ED \u0159\u00EDd\u00EDc\u00ED po\u010D\u00EDta\u010D"@cs . . . . "Dlouh\u00FD pochod 1D"@cs . "28220.0"^^ . "1"^^ . "81650.0"^^ . . "Retired" . "81650000.0"^^ . .