medium-lift launch vehicle
From Spacefaring
Q22906832
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.
Wikimedia, Wikidata
MLLV; MLV
payload mass 2000 kilogram, payload mass 20000 kilogram, payload mass 5000 kilogram,
Kvant, Cyclone-4M, Delta III, Delta II, Delta IV, Dong Fang Hong 2, Ekran, H3 Launch Vehicle, H-II, Atlas V, Launch Vehicle Mark III, launch vehicle, Neutron, Pallas-1, Republic of Haiti, Zhuque-2, Firefly Eclipse, Falcon 9, Atlas II, Atlas III, Atlas IIAS, Atlas IIA, Tarshish, Sweden, Sikh Confederacy, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, Ashkenaz,
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Location: KML, Cluster Map, Maps,
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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
| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| class | rocket | Atlas III | Atlas, medium-lift launch vehicle | Wikidata | |
| class | rocket | Atlas V | Atlas, medium-lift launch vehicle | Wikidata | |
| class | rocket | Cyclone-4M | medium-lift launch vehicle, liquid-propellant rocket, two-stage-to-orbit, expendable launch vehicle | Wikidata | |
| class | rocket | Falcon 9 | reusable launch vehicle, Falcon, medium-lift launch vehicle | Wikidata | |
| class | rocket | H-II | two-stage-to-orbit, expendable launch vehicle, liquid-propellant rocket, medium-lift launch vehicle | Wikidata | |
| class | rocket | H3 Launch Vehicle | two-stage-to-orbit, liquid-propellant rocket, medium-lift launch vehicle, expendable launch vehicle | Wikidata | |
| class | rocket | Launch Vehicle Mark III | medium-lift launch vehicle, expendable launch vehicle, three-stage-to-orbit | Wikidata | |
| class | rocket | Neutron | reusable launch vehicle, two-stage-to-orbit, medium-lift launch vehicle | Wikidata | |
| class | rocket | Pallas-1 | medium-lift launch vehicle | Wikidata | |
| class | rocket | Zhuque-2 | two-stage-to-orbit, medium-lift launch vehicle | Wikidata | |
| class | rocket | 1989 | Delta II | Delta, medium-lift launch vehicle | Wikidata |
| class | rocket | 1991 | Atlas II | Atlas, medium-lift launch vehicle | Wikidata |
| class | rocket | 1992 | Atlas IIA | Atlas, medium-lift launch vehicle | Wikidata |
| class | rocket | 1993 | Atlas IIAS | medium-lift launch vehicle, Atlas | Wikidata |
| class | rocket | 1994 | Kvant | proposed entity, medium-lift launch vehicle | Wikidata |
| class | rocket | 1998 | Delta III | Delta, medium-lift launch vehicle | Wikidata |
| class | rocket | 2002 | Delta IV | Delta, medium-lift launch vehicle | Wikidata |
| class | rocket | 2026 | Firefly Eclipse | two-stage-to-orbit, medium-lift launch vehicle, reusable launch vehicle | Wikidata |