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Statements

Subject Item
dbr:Delta-K
rdf:type
dbo:Person yago:Phase115290337 yago:WikicatRocketStages yago:FundamentalQuantity113575869 yago:TimePeriod115113229 yago:Measure100033615 yago:Abstraction100002137
rdfs:label
Delta-K Delta-K Delta-K Delta K
rdfs:comment
The Delta-K was an American rocket stage, developed by McDonnell Douglas and Aerojet. It was first used on 27 August 1989 as the second stage for the Delta 4000 series. It continued to serve as the second stage for subsequent variants of the Delta rocket. It was propelled by a single AJ10-118K rocket engine, fueled by Aerozine 50 and dinitrogen tetroxide, which are hypergolic. As of 25 May 2008, 138 have been launched, and excluding one which was destroyed by the explosion of a lower stage, none have failed. Delta-K merupakan tahapan roket Amerika, yang dikembangkan oleh McDonnell Douglas dan Aerojet. Ini pertama kali digunakan pada 27 Agustus 1989 sebagai tahap kedua untuk seri Delta 4000. Delta-K masih digunakan, saat ini sebagai tahap kedua dari roket Delta II. Delta-K – górny człon rakiet Delta 3000, Delta 4000, Delta 5000 i Delta II. W przeciwieństwie do innych stopni serii Delta napędzanych silnikiem AJ-10 różnił się rodzajem paliwa. Zamiast mieszanki UDMH i HNO3 wykorzystywał mieszaninę Aerozine 50 i N2O4. O Delta K é um foguete espacial estadunidense usado como estágio de vários outros foguetes Delta.
foaf:depiction
n15:Delta-II_Stage2_XSS-10.jpg
dcterms:subject
dbc:Rocket_stages
dbo:wikiPageID
17602697
dbo:wikiPageRevisionID
1064564748
dbo:wikiPageWikiLink
dbr:Advanced_Common_Evolved_Stage dbr:Rocket dbr:UDMH dbc:Rocket_stages dbr:Boeing dbr:Hypergolic dbr:AJ-10 dbr:United_Launch_Alliance dbr:Able_(rocket_stage) dbr:Delta_4000 dbr:Vanguard_rocket dbr:Delta_5000 dbr:Delta_Cryogenic_Second_Stage dbr:McDonnell_Douglas dbr:Aerozine_50 dbr:Transtage dbr:Delta_rocket dbr:Dinitrogen_tetroxide dbr:Upper_stage dbr:Nitric_acid dbr:Vanguard_(rocket) dbr:ICESat-2 dbr:Vanguard_1 dbr:Delta_II
owl:sameAs
wikidata:Q49548 freebase:m.0464jz4 yago-res:Delta-K dbpedia-pl:Delta-K dbpedia-bg:Делта-К dbpedia-pt:Delta_K n21:4bBxy dbpedia-id:Delta-K dbpedia-gl:Delta_K
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dbt:Upper_stages dbt:Use_dmy_dates dbt:Infobox_rocket_stage dbt:N2O4 n23:stage dbt:Reflist dbt:Convert dbt:Rocket-stub
dbo:thumbnail
n15:Delta-II_Stage2_XSS-10.jpg?width=300
dbp:caption
Spent Delta-K stage, photographed in orbit
dbp:manufacturer
dbr:United_Launch_Alliance
dbo:abstract
The Delta-K was an American rocket stage, developed by McDonnell Douglas and Aerojet. It was first used on 27 August 1989 as the second stage for the Delta 4000 series. It continued to serve as the second stage for subsequent variants of the Delta rocket. It was propelled by a single AJ10-118K rocket engine, fueled by Aerozine 50 and dinitrogen tetroxide, which are hypergolic. The Delta-K had a long heritage to the first Able stage used in Project Vanguard. The AJ-10 engine was first used in the Able second stage of the Vanguard rocket, as the AJ10-118 configuration. It was initially fueled by nitric acid and UDMH. An AJ10 engine was first fired in flight during the third Vanguard launch, on 17 March 1958, which successfully placed the Vanguard 1 satellite into orbit. As of 25 May 2008, 138 have been launched, and excluding one which was destroyed by the explosion of a lower stage, none have failed. The Delta-K was used as the second stage of the Delta II rocket from 1989 to 2018. This second stage was retired at conclusion of the ICESat-2 launch on 15 September 2018. O Delta K é um foguete espacial estadunidense usado como estágio de vários outros foguetes Delta. Delta-K merupakan tahapan roket Amerika, yang dikembangkan oleh McDonnell Douglas dan Aerojet. Ini pertama kali digunakan pada 27 Agustus 1989 sebagai tahap kedua untuk seri Delta 4000. Delta-K masih digunakan, saat ini sebagai tahap kedua dari roket Delta II. Delta-K – górny człon rakiet Delta 3000, Delta 4000, Delta 5000 i Delta II. W przeciwieństwie do innych stopni serii Delta napędzanych silnikiem AJ-10 różnił się rodzajem paliwa. Zamiast mieszanki UDMH i HNO3 wykorzystywał mieszaninę Aerozine 50 i N2O4.
dbp:countryOrigin
United States
dbp:rockets
dbr:Delta_4000 dbr:Delta_5000 dbr:Delta_II
gold:hypernym
dbr:Stage
prov:wasDerivedFrom
wikipedia-en:Delta-K?oldid=1064564748&ns=0
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3380
foaf:isPrimaryTopicOf
wikipedia-en:Delta-K