Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/Boost_phase> ?p ?o }
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- Boost_phase abstract "The boost phase is the portion of the flight of a ballistic missile or space vehicle during which the booster and sustainer engines operate until it reaches peak velocity. This phase can take 3 to 4 minutes (for a solid rocket shorter than for a liquid-propellant rocket), the altitude at the end of this phase is 150–200 km, and the typical burn-out speed is 7 km/s. Boost-phase intercept is a type of missile defense technology that would be designed to disable enemy missiles while they are still in the boost phase.".
- Boost_phase wikiPageID "2691856".
- Boost_phase wikiPageLength "864".
- Boost_phase wikiPageOutDegree "9".
- Boost_phase wikiPageRevisionID "654729783".
- Boost_phase wikiPageWikiLink Altitude.
- Boost_phase wikiPageWikiLink Ballistic_missile.
- Boost_phase wikiPageWikiLink Boost-phase_intercept.
- Boost_phase wikiPageWikiLink Booster_(rocketry).
- Boost_phase wikiPageWikiLink Category:Ballistic_missiles.
- Boost_phase wikiPageWikiLink Category:Flight_phases.
- Boost_phase wikiPageWikiLink Liquid_rocket_propellant.
- Boost_phase wikiPageWikiLink Liquid_rocket_propellants.
- Boost_phase wikiPageWikiLink Missile_defense.
- Boost_phase wikiPageWikiLink Solid-fuel_rocket.
- Boost_phase wikiPageWikiLink Solid_rocket.
- Boost_phase wikiPageWikiLinkText "ascent phase".
- Boost_phase wikiPageWikiLinkText "boost phase".
- Boost_phase hasPhotoCollection Boost_phase.
- Boost_phase wikiPageUsesTemplate Template:Reflist.
- Boost_phase wikiPageUsesTemplate Template:Rocket-stub.
- Boost_phase subject Category:Ballistic_missiles.
- Boost_phase subject Category:Flight_phases.
- Boost_phase hypernym Portion.
- Boost_phase type AnatomicalStructure.
- Boost_phase comment "The boost phase is the portion of the flight of a ballistic missile or space vehicle during which the booster and sustainer engines operate until it reaches peak velocity. This phase can take 3 to 4 minutes (for a solid rocket shorter than for a liquid-propellant rocket), the altitude at the end of this phase is 150–200 km, and the typical burn-out speed is 7 km/s.".
- Boost_phase label "Boost phase".
- Boost_phase sameAs m.07y8tn.
- Boost_phase sameAs Активный_участок_полёта.
- Boost_phase sameAs Q4060117.
- Boost_phase sameAs Q4060117.
- Boost_phase wasDerivedFrom Boost_phase?oldid=654729783.
- Boost_phase isPrimaryTopicOf Boost_phase.