medium-lift launch vehicle

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Q22906832




A medium-lift launch vehicle (MLV) is a rocket launch vehicle that is capable of lifting between 2,000 to 20,000 kg by NASA classification or between 5,000 to 20,000 kilograms by Russian classification of payload into low Earth orbit (LEO). An MLV is between a small-lift launch vehicle and a heavy-lift launch vehicle. Medium-lift vehicles comprise the majority of orbital launches as of 2024, with both the Soyuz and Falcon 9 having launched several hundred times.

WikimediaWikidata
MLLV; MLV
payload mass 2000 kilogram, payload mass 20000 kilogram, payload mass 5000 kilogram, 
launch vehicle
KvantCyclone-4MDelta IIIDelta IIDelta IVDong Fang Hong 2EkranH3 Launch VehicleH-IIAtlas VLaunch Vehicle Mark IIIlaunch vehicleNeutronPallas-1Republic of HaitiZhuque-2Firefly EclipseFalcon 9Atlas IIAtlas IIIAtlas IIASAtlas IIATarshishSwedenSikh ConfederacyPersiaKingdom of WolaitaKingdom of Martabam-hongsawatoiHavilahDemocratic Republic of the CongoChinlandCalvinist Republic of GhentAshkenaz

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Location: KML, Cluster Map, Maps,

  • Atlas III
    series of American expendable launch system
  • Atlas V
    American expendable launch system
  • Cyclone-4M
    proposed Ukrainian expendable launch vehicle
  • Falcon 9
    partially reusable orbital launch vehicle by SpaceX
  • H-II
    Japanese family of rockets
  • H3 Launch Vehicle
    Japanese expendable launch system
  • Launch Vehicle Mark III
    launch vehicle developed by the Indian Space Research Organisation
  • Neutron
    orbital launch vehicle under development by Rocket Lab
  • Pallas-1
    partially reusable orbital launch vehicle by Galactic Energy
  • Zhuque-2
    orbital medium-lift launch vehicle from the Chinese company LandSpace
  • Delta II
    retired expendable launch system in the Delta rocket family
  • Atlas II
    American expendable launch system
  • Atlas IIA
    American expendable launch system
  • Atlas IIAS
    American expendable launch system
  • Kvant
    proposed Russian launch vehicle
  • Delta III
    retired expendable launch system in the Delta rocket family
  • Delta IV
    expendable launch system in the Delta rocket family
  • Firefly Eclipse
    proposed two-stage orbital launch vehicle
    TypeSubtypeDateDescriptionNotesSource
    classrocketAtlas IIIAtlas, medium-lift launch vehicleWikidata
    classrocketAtlas VAtlas, medium-lift launch vehicleWikidata
    classrocketCyclone-4Mmedium-lift launch vehicle, liquid-propellant rocket, two-stage-to-orbit, expendable launch vehicleWikidata
    classrocketFalcon 9reusable launch vehicle, Falcon, medium-lift launch vehicleWikidata
    classrocketH-IItwo-stage-to-orbit, expendable launch vehicle, liquid-propellant rocket, medium-lift launch vehicleWikidata
    classrocketH3 Launch Vehicletwo-stage-to-orbit, liquid-propellant rocket, medium-lift launch vehicle, expendable launch vehicleWikidata
    classrocketLaunch Vehicle Mark IIImedium-lift launch vehicle, expendable launch vehicle, three-stage-to-orbitWikidata
    classrocketNeutronreusable launch vehicle, two-stage-to-orbit, medium-lift launch vehicleWikidata
    classrocketPallas-1medium-lift launch vehicleWikidata
    classrocketZhuque-2two-stage-to-orbit, medium-lift launch vehicleWikidata
    classrocket1989Delta IIDelta, medium-lift launch vehicleWikidata
    classrocket1991Atlas IIAtlas, medium-lift launch vehicleWikidata
    classrocket1992Atlas IIAAtlas, medium-lift launch vehicleWikidata
    classrocket1993Atlas IIASmedium-lift launch vehicle, AtlasWikidata
    classrocket1994Kvantproposed entity, medium-lift launch vehicleWikidata
    classrocket1998Delta IIIDelta, medium-lift launch vehicleWikidata
    classrocket2002Delta IVDelta, medium-lift launch vehicleWikidata
    classrocket2026Firefly Eclipsetwo-stage-to-orbit, medium-lift launch vehicle, reusable launch vehicleWikidata