Matches in DBpedia 2014 for { <http://dbpedia.org/resource/VLM_(rocket)> ?p ?o. }
Showing items 1 to 65 of
65
with 100 items per page.
- VLM_(rocket) diameter "1.5".
- VLM_(rocket) lowerEarthOrbitPayload "200.0".
- VLM_(rocket) abstract "The VLM (Veículo Lançador de Microssatélites) is a proposed Brazilian satellite launcher. The project originated as a simplified version of the VLS-1 rocket, using only the core stages.Currently, a version based on the S50 rocket engine is being studied, with the objective of orbiting satellites up to 150 kg in circular orbits ranging from 250 to 700 km. It will be a three stage rocket, expected to launch the SHEFEX III mission by the German Aerospace Center (DLR) in 2016.".
- VLM_(rocket) countryOrigin Brazil.
- VLM_(rocket) diameter "1.5".
- VLM_(rocket) launchSite Alc%C3%A2ntara_Launch_Center.
- VLM_(rocket) lowerEarthOrbitPayload "200000.0".
- VLM_(rocket) manufacturer Aerospace_Technology_and_Science_Department.
- VLM_(rocket) rocketFunction Launch_vehicle.
- VLM_(rocket) rocketStages "3".
- VLM_(rocket) status "In development".
- VLM_(rocket) wikiPageID "36191352".
- VLM_(rocket) wikiPageRevisionID "556621742".
- VLM_(rocket) altStage3thrust "7473".
- VLM_(rocket) caption "The two projected VLM configurations".
- VLM_(rocket) diameter "1.5 m".
- VLM_(rocket) first "2015".
- VLM_(rocket) function "Orbital launch vehicle".
- VLM_(rocket) hasPhotoCollection VLM_(rocket).
- VLM_(rocket) leoPayload "200.0".
- VLM_(rocket) manufacturer Aerospace_Technology_and_Science_Department.
- VLM_(rocket) name "VLM-1".
- VLM_(rocket) name "Veículo Lançador de Microssatélites".
- VLM_(rocket) sites Centro_de_Lançamento_de_Alcântara.
- VLM_(rocket) stage1engines "1".
- VLM_(rocket) stage1fuel Solid-fuel_rocket.
- VLM_(rocket) stage1name "S-50".
- VLM_(rocket) stage1si "277.0".
- VLM_(rocket) stage1thrust "~400 kN".
- VLM_(rocket) stage1time "60.0".
- VLM_(rocket) stage2engines "1".
- VLM_(rocket) stage2fuel Solid-fuel_rocket.
- VLM_(rocket) stage2name "S-50".
- VLM_(rocket) stage2si "277.0".
- VLM_(rocket) stage2thrust "~400 kN".
- VLM_(rocket) stage2time "60.0".
- VLM_(rocket) stage3engines "1".
- VLM_(rocket) stage3fuel Solid-fuel_rocket.
- VLM_(rocket) stage3name "S-44".
- VLM_(rocket) stage3si "282.0".
- VLM_(rocket) stage3thrust "33.24 kN".
- VLM_(rocket) stage3time "68.0".
- VLM_(rocket) stages "3".
- VLM_(rocket) status "In development".
- VLM_(rocket) subject Category:Expendable_space_launch_systems.
- VLM_(rocket) subject Category:Rockets_and_missiles.
- VLM_(rocket) subject Category:Science_and_technology_in_Brazil.
- VLM_(rocket) subject Category:Space_launch_vehicles_of_Brazil.
- VLM_(rocket) subject Category:Space_program_of_Brazil.
- VLM_(rocket) type MeanOfTransportation.
- VLM_(rocket) type Rocket.
- VLM_(rocket) type DesignedArtifact.
- VLM_(rocket) comment "The VLM (Veículo Lançador de Microssatélites) is a proposed Brazilian satellite launcher. The project originated as a simplified version of the VLS-1 rocket, using only the core stages.Currently, a version based on the S50 rocket engine is being studied, with the objective of orbiting satellites up to 150 kg in circular orbits ranging from 250 to 700 km. It will be a three stage rocket, expected to launch the SHEFEX III mission by the German Aerospace Center (DLR) in 2016.".
- VLM_(rocket) label "VLM (rocket)".
- VLM_(rocket) label "Veículo Lançador de Microssatélite".
- VLM_(rocket) label "Véhicule lanceur de micro-satellites".
- VLM_(rocket) sameAs Véhicule_lanceur_de_micro-satellites.
- VLM_(rocket) sameAs Veículo_Lançador_de_Microssatélite.
- VLM_(rocket) sameAs m.0k0tpvf.
- VLM_(rocket) sameAs Q7907157.
- VLM_(rocket) sameAs Q7907157.
- VLM_(rocket) wasDerivedFrom VLM_(rocket)?oldid=556621742.
- VLM_(rocket) isPrimaryTopicOf VLM_(rocket).
- VLM_(rocket) name "VLM-1".
- VLM_(rocket) name "Veículo Lançador de Microssatélites".