DBpedia – Linked Data Fragments

Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/Long_March_1D> ?p ?o }

• Long_March_1D diameter "2.25".
• Long_March_1D height "28220.0".
• Long_March_1D mass "81650.0".
• Long_March_1D mass "81650.0".
• Long_March_1D abstract "During the 1990's CALT developed an improved version of the DF-4 to test the reentry vehicle warheads of the DF-31. They took advantage of this development and offered it as the Long March 1D for commercial application. The modification included: An DF-4 improved first stage, which used the new version of the YF-2B, and switched propellants to UDMH/N2O4 for improved performance. The use switch of the second stage YF-3A, for the Long March 4 third stage engine, the YF-40. A new, cylinder interstage between the second and third stage, which enabled to add RCS to the third stage. The olde one was tapered. A new third stage with a new motor, the FG-36 and an optional RCS. A new computer inertial guidance system which enabled the third stage to be 3-axis stabilized for added precision.The new design did not had a good reception and was only used for reentry vehicle tests. It flew three suborbital missions from Taiyuan LC-1 with two successes and a failure on the final mission. The first launch was on June 1, 1995 and the second one was on November of 1997. The final and failed on was on January 3, 2002.".
• Long_March_1D comparable Mu_(rocket_family).
• Long_March_1D countryOrigin China.
• Long_March_1D diameter "2.25".
• Long_March_1D failedLaunches "1".
• Long_March_1D finalFlight "2002-01-03".
• Long_March_1D height "28.22".
• Long_March_1D launchSite Taiyuan_Satellite_Launch_Center.
• Long_March_1D maidenFlight "1995-06-01".
• Long_March_1D manufacturer China_Academy_of_Launch_Vehicle_Technology.
• Long_March_1D mass "8.165E7".
• Long_March_1D rocketFunction Orbital_spaceflight.
• Long_March_1D rocketStages "3".
• Long_March_1D status "Retired".
• Long_March_1D successfulLaunches "2".
• Long_March_1D totalLaunches "3".
• Long_March_1D wikiPageExternalLink www.calt.com.
• Long_March_1D wikiPageID "2892589".
• Long_March_1D wikiPageLength "9654".
• Long_March_1D wikiPageOutDegree "39".
• Long_March_1D wikiPageRevisionID "673492175".
• Long_March_1D wikiPageWikiLink Atmospheric_entry.
• Long_March_1D wikiPageWikiLink Category:Long_March_(rocket_family).
• Long_March_1D wikiPageWikiLink China.
• Long_March_1D wikiPageWikiLink China_Academy_of_Launch_Vehicle_Technology.
• Long_March_1D wikiPageWikiLink DF-31.
• Long_March_1D wikiPageWikiLink DF-4.
• Long_March_1D wikiPageWikiLink Dinitrogen_tetroxide.
• Long_March_1D wikiPageWikiLink FG-36.
• Long_March_1D wikiPageWikiLink Hydrazine.
• Long_March_1D wikiPageWikiLink Hydroxyl-terminated_polybutadiene.
• Long_March_1D wikiPageWikiLink Launch_vehicle.
• Long_March_1D wikiPageWikiLink Long_March_(rocket_family).
• Long_March_1D wikiPageWikiLink Long_March_1_(rocket_family).
• Long_March_1D wikiPageWikiLink Long_March_4_(rocket_family).
• Long_March_1D wikiPageWikiLink Low_Earth_orbit.
• Long_March_1D wikiPageWikiLink Monopropellant_rocket.
• Long_March_1D wikiPageWikiLink Mu_(rocket_family).
• Long_March_1D wikiPageWikiLink Orbital_spaceflight.
• Long_March_1D wikiPageWikiLink Reaction_control_system.
• Long_March_1D wikiPageWikiLink Solid-fuel_rocket.
• Long_March_1D wikiPageWikiLink Taiyuan_Launch_Complex_1.
• Long_March_1D wikiPageWikiLink Taiyuan_Satellite_Launch_Center.
• Long_March_1D wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
• Long_March_1D wikiPageWikiLink YF-1.
• Long_March_1D wikiPageWikiLink YF-40.
• Long_March_1D wikiPageWikiLinkText "CZ-1D".
• Long_March_1D wikiPageWikiLinkText "Long March 1D".
• Long_March_1D comparable Mu_(rocket_family).
• Long_March_1D countryOrigin China.
• Long_March_1D fail "1".
• Long_March_1D family "--03-01".
• Long_March_1D first "1995-06-01".
• Long_March_1D function Launch_vehicle.
• Long_March_1D function Orbital_spaceflight.
• Long_March_1D hasPhotoCollection Long_March_1D.
• Long_March_1D last "2002-01-03".
• Long_March_1D launches "3".
• Long_March_1D manufacturer China_Academy_of_Launch_Vehicle_Technology.
• Long_March_1D name "--03-01".
• Long_March_1D payloads Atmospheric_entry.
• Long_March_1D sites Taiyuan_Launch_Complex_1.
• Long_March_1D sites Taiyuan_Satellite_Launch_Center.
• Long_March_1D stages "3".
• Long_March_1D status "Retired".
• Long_March_1D success "2".
• Long_March_1D wikiPageUsesTemplate Template:China-stub.
• Long_March_1D wikiPageUsesTemplate Template:Chinese_space_program.
• Long_March_1D wikiPageUsesTemplate Template:Expendable_launch_systems.
• Long_March_1D wikiPageUsesTemplate Template:Infobox_rocket.
• Long_March_1D wikiPageUsesTemplate Template:Long_March_rockets.
• Long_March_1D wikiPageUsesTemplate Template:Reflist.
• Long_March_1D wikiPageUsesTemplate Template:Rocket-stub.
• Long_March_1D subject Category:Long_March_(rocket_family).
• Long_March_1D type Article.
• Long_March_1D type MeanOfTransportation.
• Long_March_1D type Rocket.
• Long_March_1D type Article.
• Long_March_1D type Vehicle.
• Long_March_1D type DesignedArtifact.
• Long_March_1D type Thing.
• Long_March_1D type Q41291.
• Long_March_1D comment "During the 1990's CALT developed an improved version of the DF-4 to test the reentry vehicle warheads of the DF-31. They took advantage of this development and offered it as the Long March 1D for commercial application. The modification included: An DF-4 improved first stage, which used the new version of the YF-2B, and switched propellants to UDMH/N2O4 for improved performance. The use switch of the second stage YF-3A, for the Long March 4 third stage engine, the YF-40.".
• Long_March_1D label "Long March 1D".
• Long_March_1D sameAs Long_March_1D.
• Long_March_1D sameAs Longa_Marcha_1D.
• Long_March_1D sameAs m.089my1.
• Long_March_1D sameAs Великий_поход-1D.
• Long_March_1D sameAs Q6672966.
• Long_March_1D sameAs Q6672966.
• Long_March_1D sameAs 長征一號丁運載火箭.
• Long_March_1D wasDerivedFrom Long_March_1D?oldid=673492175.
• Long_March_1D isPrimaryTopicOf Long_March_1D.
• Long_March_1D name "Long March 1D".