Matches in DBpedia 2016-04 for { <http://wikidata.dbpedia.org/resource/Q22978> ?p ?o }
Showing triples 1 to 61 of
61
with 100 triples per page.
- Q22978 subject Q8274952.
- Q22978 abstract "The Atlas I was an American expendable launch system, used in the 1990s to launch a variety of different satellites. The "I" in "Atlas I" can cause confusion, as all previous Atlas rockets were designated using letters, ending with the Atlas H, however subsequent rockets were designated using Roman numerals, starting with the Atlas II. Officially, the "I" is the Roman numeral "1".The first stage of the Atlas I was derived from Atlas G, and the second stage was a Centaur. The first stage had an improved MA-5A propulsion system, consisting of the LR-89 booster engine with dual thrust chambers and a more powerful RS-27 replacing the traditional LR-105 sustainer engine. With the new RS-27 sustainer engine, all three of the large Atlas thrust chambers produced equal thrust. Booster engine jettison occurred prior to sustainer engine cut-off for stage-and-a-half staging of the Atlas. (Used in conjunction with the Centaur, this gave the Atlas I 2.5 stages).".
- Q22978 countryOrigin Q30.
- Q22978 diameter "3.05".
- Q22978 failedLaunches "3".
- Q22978 finalFlight "1997-04-25".
- Q22978 height "43.9".
- Q22978 launchSite Q334465.
- Q22978 launchSite Q672830.
- Q22978 maidenFlight "1990-07-25".
- Q22978 manufacturer Q836947.
- Q22978 mass "1.643E8".
- Q22978 rocketFunction Q15078724.
- Q22978 rocketStages "3".
- Q22978 status "Retired".
- Q22978 successfulLaunches "8".
- Q22978 thumbnail Atlas_I_launching_CRRES_satellite1.jpg?width=300.
- Q22978 totalLaunches "11".
- Q22978 wikiPageWikiLink Q1161829.
- Q22978 wikiPageWikiLink Q15078724.
- Q22978 wikiPageWikiLink Q198107.
- Q22978 wikiPageWikiLink Q22949.
- Q22978 wikiPageWikiLink Q23600.
- Q22978 wikiPageWikiLink Q23770.
- Q22978 wikiPageWikiLink Q30.
- Q22978 wikiPageWikiLink Q334465.
- Q22978 wikiPageWikiLink Q5013937.
- Q22978 wikiPageWikiLink Q5155949.
- Q22978 wikiPageWikiLink Q5518095.
- Q22978 wikiPageWikiLink Q6288445.
- Q22978 wikiPageWikiLink Q672830.
- Q22978 wikiPageWikiLink Q761888.
- Q22978 wikiPageWikiLink Q8274952.
- Q22978 wikiPageWikiLink Q836947.
- Q22978 wikiPageWikiLink Q862610.
- Q22978 wikiPageWikiLink Q976688.
- Q22978 countryOrigin Q30.
- Q22978 diameter "3.05m".
- Q22978 fail "3".
- Q22978 first "1990-07-25".
- Q22978 function Q15078724.
- Q22978 height "43.90m".
- Q22978 last "1997-04-25".
- Q22978 launches "11".
- Q22978 manufacturer Q836947.
- Q22978 mass "164300.0".
- Q22978 name "Atlas I".
- Q22978 sites Q334465.
- Q22978 sites Q672830.
- Q22978 stages "2.5".
- Q22978 status "Retired".
- Q22978 success "8".
- Q22978 type MeanOfTransportation.
- Q22978 type Rocket.
- Q22978 type DesignedArtifact.
- Q22978 type Thing.
- Q22978 type Q41291.
- Q22978 comment "The Atlas I was an American expendable launch system, used in the 1990s to launch a variety of different satellites. The "I" in "Atlas I" can cause confusion, as all previous Atlas rockets were designated using letters, ending with the Atlas H, however subsequent rockets were designated using Roman numerals, starting with the Atlas II. Officially, the "I" is the Roman numeral "1".The first stage of the Atlas I was derived from Atlas G, and the second stage was a Centaur.".
- Q22978 label "Atlas I".
- Q22978 depiction Atlas_I_launching_CRRES_satellite1.jpg.
- Q22978 name "Atlas I".