Matches in DBpedia 2016-04 for { <http://wikidata.dbpedia.org/resource/Q548376> ?p ?o }
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- Q548376 subject Q7016480.
- Q548376 subject Q7016482.
- Q548376 abstract "The H-II (H2) rocket was a Japanese satellite launch system, which flew seven times between 1994 and 1999, with five successes. It was developed by NASDA in order to give Japan a capability to launch larger satellites in the 1990s. It was the first two-stage liquid-fuelled rocket Japan made using only technologies developed domestically. It was superseded by the H-IIA rocket following reliability and cost issues.".
- Q548376 countryOrigin Q17.
- Q548376 diameter "4.0".
- Q548376 failedLaunches "1".
- Q548376 finalFlight "1999-11-15".
- Q548376 height "49.0".
- Q548376 launchSite Q5656106.
- Q548376 launchSite Q742683.
- Q548376 lowerEarthOrbitPayload "1.006E7".
- Q548376 maidenFlight "1994-02-03".
- Q548376 manufacturer Q648280.
- Q548376 mass "2.6E8".
- Q548376 partialFailedLaunches "1".
- Q548376 rocketFunction Q697175.
- Q548376 rocketStages "2".
- Q548376 status "Retired".
- Q548376 successfulLaunches "5".
- Q548376 thumbnail H-ii_adeos.gif?width=300.
- Q548376 totalLaunches "7".
- Q548376 wikiPageExternalLink index_e.html.
- Q548376 wikiPageWikiLink Q100995.
- Q548376 wikiPageWikiLink Q1050451.
- Q548376 wikiPageWikiLink Q1054827.
- Q548376 wikiPageWikiLink Q1072125.
- Q548376 wikiPageWikiLink Q1138649.
- Q548376 wikiPageWikiLink Q12438.
- Q548376 wikiPageWikiLink Q1279552.
- Q548376 wikiPageWikiLink Q131535.
- Q548376 wikiPageWikiLink Q14927.
- Q548376 wikiPageWikiLink Q1536.
- Q548376 wikiPageWikiLink Q1586339.
- Q548376 wikiPageWikiLink Q1627566.
- Q548376 wikiPageWikiLink Q17.
- Q548376 wikiPageWikiLink Q2001116.
- Q548376 wikiPageWikiLink Q2611697.
- Q548376 wikiPageWikiLink Q26540.
- Q548376 wikiPageWikiLink Q266487.
- Q548376 wikiPageWikiLink Q2704796.
- Q548376 wikiPageWikiLink Q280602.
- Q548376 wikiPageWikiLink Q30.
- Q548376 wikiPageWikiLink Q3103808.
- Q548376 wikiPageWikiLink Q3658287.
- Q548376 wikiPageWikiLink Q4390199.
- Q548376 wikiPageWikiLink Q472251.
- Q548376 wikiPageWikiLink Q49506.
- Q548376 wikiPageWikiLink Q506691.
- Q548376 wikiPageWikiLink Q5155949.
- Q548376 wikiPageWikiLink Q5656106.
- Q548376 wikiPageWikiLink Q570607.
- Q548376 wikiPageWikiLink Q60580.
- Q548376 wikiPageWikiLink Q60599.
- Q548376 wikiPageWikiLink Q618153.
- Q548376 wikiPageWikiLink Q622779.
- Q548376 wikiPageWikiLink Q648280.
- Q548376 wikiPageWikiLink Q663611.
- Q548376 wikiPageWikiLink Q697175.
- Q548376 wikiPageWikiLink Q7016480.
- Q548376 wikiPageWikiLink Q7016482.
- Q548376 wikiPageWikiLink Q742683.
- Q548376 wikiPageWikiLink Q860308.
- Q548376 countryOrigin Q17.
- Q548376 diameter "4 m".
- Q548376 fail "1".
- Q548376 first "1994-02-03".
- Q548376 function Q697175.
- Q548376 height "49 m".
- Q548376 last "1999-11-15".
- Q548376 launches "7".
- Q548376 leoPayload "10060.0".
- Q548376 manufacturer Q648280.
- Q548376 mass "260000.0".
- Q548376 name "H-II".
- Q548376 partial "1".
- Q548376 sites Q5656106.
- Q548376 sites Q742683.
- Q548376 stages "2".
- Q548376 status "Retired".
- Q548376 success "5".
- Q548376 type MeanOfTransportation.
- Q548376 type Rocket.
- Q548376 type DesignedArtifact.
- Q548376 type Thing.
- Q548376 type Q41291.
- Q548376 comment "The H-II (H2) rocket was a Japanese satellite launch system, which flew seven times between 1994 and 1999, with five successes. It was developed by NASDA in order to give Japan a capability to launch larger satellites in the 1990s. It was the first two-stage liquid-fuelled rocket Japan made using only technologies developed domestically. It was superseded by the H-IIA rocket following reliability and cost issues.".
- Q548376 label "H-II".
- Q548376 depiction H-ii_adeos.gif.
- Q548376 name "H-II".