Delta 1000 (original) (raw)
Delta seri 1000 (juga disebut sebagai Straight-Eight) adalah sistem peluncuran expendable (sekali pakai) Amerika yang digunakan untuk melakukan peluncuran delapan orbital antara tahun 1972 dan 1975. Itu adalah anggota keluarga roket Delta. Beberapa varian ada, dibedakan oleh empat kode numerik digit.
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| dbo:abstract | The Delta 1000 series (also referred to as Straight-Eight) was an American expendable launch system which was used to conduct eight orbital launches between 1972 and 1975. It was a member of the Delta family of rockets. Several variants existed, differentiated by a four digit numerical code. Delta 1000 was developed by McDonnell Douglas company (now — Boeing) in 1972. The same first stage and boosters were used on all variants. The first stage was an , a further stretched version of the used on earlier versions, itself derived from the Thor missile. Four, six or nine Castor-2 solid rocket boosters were attached to increase thrust at lift-off. These improvements permitted the Delta 1000 series to lift 1,835 kg (4,045 lbs) to LEO or 635 kg (1,400 lbs) to GTO. The nickname "Straight-Eight" comes from the fact that its second stage variants had the same 8 ft. (2.4 m) diameter as the first stage; previous Delta second stages were smaller in diameter. Two different second stages were flown, depending on the variant: * The second stage, featuring the Aerojet AJ10-118G engine, was flown on three launches, with Explorer 47, 50 and 51; the Aerojet engine was flown for the (Anik A1) satellite launch (mistakenly marked as xx1x in Delta 1000 series) * The Delta-P second stage, featuring the new TRW TR-201 engine, was used for two launches each in 1973 and 1975. Some flights used a third stage, either the Thiokol Star-37D or Star-37E, for launches beyond low Earth orbit. One probe launched by the Delta 1000 series, Delta 1913, was Explorer 49 that was placed into lunar orbit on 10 June 1973. Delta 1000 rockets were launched from Space Launch Complex 2W at Vandenberg AFB and Launch Complex 17B at Cape Canaveral. All eight (1972-1975) launches were successful. Launching from LC-17B was had resulted successful removal of the exploitor-47 spacecraft for the study of the Earth's magnetosphere. During the first stage a carrier rocket was used in the modification of Delta-1604 with the onboard number 579/D90. The Japanese N-II and H-I launch vehicles used the same Extended Long Tank Thor first stage. For the second stage, the N-II used the Delta-F while the H-I had the Japanese LE-5 engine which used liquid hydrogen and oxygen. (en) Delta seri 1000 (juga disebut sebagai Straight-Eight) adalah sistem peluncuran expendable (sekali pakai) Amerika yang digunakan untuk melakukan peluncuran delapan orbital antara tahun 1972 dan 1975. Itu adalah anggota keluarga roket Delta. Beberapa varian ada, dibedakan oleh empat kode numerik digit. (in) Delta 1000 – seria amerykańskich rakiet nośnych Delta, oblatana w latach 1972–1975. Była to pierwsza seria rakiet Delta wykorzystująca stopień Thor ELT, będący wydłużoną do 22,4 m wersją rakiety Thor. Część rakiet tej serii uzyskała nazwę Straight Eight (dosłownie: prosta ósemka). Nazwa ta odnosiła się do średnicy drugiego stopnia rakiety oraz przestrzeni ładunkowej, wynoszącej 8 stóp (ok. 2,44 m), czyli tyle samo co centralny człon rakiety. (pl) Delta 1000 foi uma série de foguetes espaciais estadunidense que prestou serviço na década de 1970. A série 1000 era composta pelos Delta 1410, Delta 1604, Delta 1900, Delta 1910, Delta 1913 e Delta 1914, de acordo com o sistema de numeração seguido pela família de foguetes Delta. (pt) «Дельта-1000» (также Straight-Eight) — американская трёхступенчатая ракета-носитель среднего класса, семейства Дельта, разработки компании McDonnell Douglas (ныне — Boeing) в 1972 году. Первый пуск ракеты-носителя Дельта-1000 был осуществлён 23 сентября 1972 года со стартовой площадки LC-17B космодрома Канаверал. Результатом пуска было успешное выведение на НОО космического аппарата для изучения магнитосферы Земли. Во время пуска использовалась ракета-носитель в модификации Дельта-1604 с бортовым номером 579/D90. Всего было осуществлено 8 пусков в период с 1972 года по 1975 год. (ru) 三角洲1000系列（英語：Delta 1000），又稱為直八（英語：Straight-Eight），是美國的，在1972年到1975年之間曾進行過8次軌道發射。它是三角洲系列運載火箭家族的成員。存在幾種變體，以四位數數字代碼區分。 相同的第一階段和助推器用於所有變體。第一階段是，這是早期版本使用的的進一步延伸版本，其本身是從衍生而來的。附加了四個，六個或九個固體火箭助推器，以增加起飛時的推力。這些改進使Delta 1000系列可以將1,835千克（4,045磅）的重量提升至LEO或將635千克（1,400磅）的重量提升至GTO。 暱稱「直八」是因為其第二級變體的直徑與第一級相同，直徑為8英尺（2.4 m）；先前的Delta第二級的直徑較小。根據不同的型號，執行了兩個不同的第二級： * 配備了Aerojet -118G發動機的第二級進行了3次發射，分別是、50和51。 （）衛星發射使用了Aerojet發動機（在Delta 1000系列中錯誤地標記為xx1x） * 第二級採用了新型TRW 發動機，分別在1973年和1975年進行了兩次發射。 一些飛行使用了第三級，即Thiokol 或，進行了低地球軌道之外的發射。由三角洲1000系列火箭Delta 1913發射的月球探測器，於1973年6月10日進入月球軌道。 三角洲1000火箭分別從范登堡空軍基地的和卡納維拉爾角空軍基地的發射，所有八次發射均成功。 (zh) |
| dbo:finalFlight | 1975-06-21 (xsd:date) |
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| dbo:maidenFlight | 1972-09-23 (xsd:date) |
| dbo:rocketFunction | dbr:Expendable_launch_system |
| dbo:status | Retired |
| dbo:successfulLaunches | 8 (xsd:nonNegativeInteger) |
| dbo:thumbnail | wiki-commons:Special:FilePath/Delta_launches_OSO_8.jpg?width=300 |
| dbo:totalLaunches | 8 (xsd:nonNegativeInteger) |
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| dbo:wikiPageRevisionID | 1084018870 (xsd:integer) |
| dbo:wikiPageWikiLink | dbr:Cape_Canaveral_Air_Force_Station dbr:Delta-P dbr:Vandenberg_AFB_Space_Launch_Complex_2 dbr:LE-5 dbr:Orbit dbr:Vandenberg_Air_Force_Base dbr:McDonnell_Douglas dbr:N-II_(rocket) dbc:Delta_(rocket_family) dbr:Delta_(rocket_family) dbr:AJ10 dbr:Explorer_47 dbr:Explorer_49 dbr:Explorer_50 dbr:Explorer_51 dbr:Anik_(satellite) dbr:PGM-17_Thor dbr:H-I dbr:TR-201 dbr:Solid_rocket_booster dbr:Expendable_launch_system dbr:Low_Earth_orbit dbr:Star_37 dbr:BOEING_Company dbr:Cape_Canaveral_Air_Force_Station_Launch_Complex_17 dbr:Booster_rocket dbr:Vandenberg_AFB dbr:Castor-2 dbr:Delta-F_(rocket_stage) dbr:Extended_Long_Tank_Thor dbr:Long_Tank_Thor dbr:OSO-8 |
| dbp:caption | Delta 1910 launching OSO-8 (en) |
| dbp:countryOrigin | United States (en) |
| dbp:first | 1972-09-23 (xsd:date) |
| dbp:function | dbr:Expendable_launch_system |
| dbp:last | 1975-06-21 (xsd:date) |
| dbp:launches | 8 (xsd:integer) |
| dbp:name | Delta 1000 series (en) |
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| dbp:status | Retired (en) |
| dbp:success | 8 (xsd:integer) |
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| dcterms:subject | dbc:Delta_(rocket_family) |
| gold:hypernym | dbr:System |
| rdf:type | owl:Thing dbo:MeanOfTransportation wikidata:Q41291 dbo:Rocket yago:Artifact100021939 yago:Conveyance103100490 yago:Instrumentality103575240 yago:Object100002684 yago:PhysicalEntity100001930 yago:Rocket104099429 yago:Vehicle104524313 yago:Whole100003553 umbel-rc:RocketEngine |
| rdfs:comment | Delta seri 1000 (juga disebut sebagai Straight-Eight) adalah sistem peluncuran expendable (sekali pakai) Amerika yang digunakan untuk melakukan peluncuran delapan orbital antara tahun 1972 dan 1975. Itu adalah anggota keluarga roket Delta. Beberapa varian ada, dibedakan oleh empat kode numerik digit. (in) Delta 1000 – seria amerykańskich rakiet nośnych Delta, oblatana w latach 1972–1975. Była to pierwsza seria rakiet Delta wykorzystująca stopień Thor ELT, będący wydłużoną do 22,4 m wersją rakiety Thor. Część rakiet tej serii uzyskała nazwę Straight Eight (dosłownie: prosta ósemka). Nazwa ta odnosiła się do średnicy drugiego stopnia rakiety oraz przestrzeni ładunkowej, wynoszącej 8 stóp (ok. 2,44 m), czyli tyle samo co centralny człon rakiety. (pl) Delta 1000 foi uma série de foguetes espaciais estadunidense que prestou serviço na década de 1970. A série 1000 era composta pelos Delta 1410, Delta 1604, Delta 1900, Delta 1910, Delta 1913 e Delta 1914, de acordo com o sistema de numeração seguido pela família de foguetes Delta. (pt) «Дельта-1000» (также Straight-Eight) — американская трёхступенчатая ракета-носитель среднего класса, семейства Дельта, разработки компании McDonnell Douglas (ныне — Boeing) в 1972 году. Первый пуск ракеты-носителя Дельта-1000 был осуществлён 23 сентября 1972 года со стартовой площадки LC-17B космодрома Канаверал. Результатом пуска было успешное выведение на НОО космического аппарата для изучения магнитосферы Земли. Во время пуска использовалась ракета-носитель в модификации Дельта-1604 с бортовым номером 579/D90. Всего было осуществлено 8 пусков в период с 1972 года по 1975 год. (ru) The Delta 1000 series (also referred to as Straight-Eight) was an American expendable launch system which was used to conduct eight orbital launches between 1972 and 1975. It was a member of the Delta family of rockets. Several variants existed, differentiated by a four digit numerical code. Delta 1000 was developed by McDonnell Douglas company (now — Boeing) in 1972. Delta 1000 rockets were launched from Space Launch Complex 2W at Vandenberg AFB and Launch Complex 17B at Cape Canaveral. All eight (1972-1975) launches were successful. (en) 三角洲1000系列（英語：Delta 1000），又稱為直八（英語：Straight-Eight），是美國的，在1972年到1975年之間曾進行過8次軌道發射。它是三角洲系列運載火箭家族的成員。存在幾種變體，以四位數數字代碼區分。 相同的第一階段和助推器用於所有變體。第一階段是，這是早期版本使用的的進一步延伸版本，其本身是從衍生而來的。附加了四個，六個或九個固體火箭助推器，以增加起飛時的推力。這些改進使Delta 1000系列可以將1,835千克（4,045磅）的重量提升至LEO或將635千克（1,400磅）的重量提升至GTO。 暱稱「直八」是因為其第二級變體的直徑與第一級相同，直徑為8英尺（2.4 m）；先前的Delta第二級的直徑較小。根據不同的型號，執行了兩個不同的第二級： * 配備了Aerojet -118G發動機的第二級進行了3次發射，分別是、50和51。 （）衛星發射使用了Aerojet發動機（在Delta 1000系列中錯誤地標記為xx1x） * 第二級採用了新型TRW 發動機，分別在1973年和1975年進行了兩次發射。 一些飛行使用了第三級，即Thiokol 或，進行了低地球軌道之外的發射。由三角洲1000系列火箭Delta 1913發射的月球探測器，於1973年6月10日進入月球軌道。 (zh) |
| rdfs:label | Delta 1000 (en) Delta 1000 (in) Delta 1000 (pl) Дельта-1000 (ru) Delta 1000 (pt) 三角洲1000 (zh) |
| owl:sameAs | freebase:Delta 1000 wikidata:Delta 1000 dbpedia-gl:Delta 1000 dbpedia-he:Delta 1000 dbpedia-id:Delta 1000 dbpedia-pl:Delta 1000 dbpedia-pt:Delta 1000 dbpedia-ru:Delta 1000 http://ta.dbpedia.org/resource/டெல்டா_1000 dbpedia-zh:Delta 1000 https://global.dbpedia.org/id/4azD2 |
| prov:wasDerivedFrom | wikipedia-en:Delta_1000?oldid=1084018870&ns=0 |
| foaf:depiction | wiki-commons:Special:FilePath/Delta_launches_OSO_8.jpg |
| foaf:isPrimaryTopicOf | wikipedia-en:Delta_1000 |
| foaf:name | Delta 1000 series (en) |
| is dbo:launchVehicle of | dbr:GEOS-3 |
| is dbo:retiredRocket of | dbr:1975_in_spaceflight |
| is dbo:wikiPageWikiLink of | dbr:Cape_Canaveral_Space_Launch_Complex_17 dbr:Delta-P dbr:Delta_4000 dbr:Descent_propulsion_system dbr:List_of_missions_to_the_Moon dbr:List_of_rockets_of_the_United_States dbr:Comparison_of_orbital_launch_systems dbr:GEOS-3 dbr:1975_in_spaceflight dbr:AJ10 dbr:Anik_(satellite) dbr:List_of_Delta_1_launches dbr:List_of_Thor_and_Delta_launches_(1970–1979) dbr:H-I dbr:HS-333 dbr:Explorers_Program dbr:Small-lift_launch_vehicle |
| is dbp:launchRocket of | dbr:GEOS-3 |
| is dbp:retired of | dbr:1975_in_spaceflight |
| is dbp:rockets of | dbr:Delta-P |
| is foaf:primaryTopic of | wikipedia-en:Delta_1000 |
