Long March 2D

E708187

Long March 2D is a Chinese two-stage orbital launch vehicle primarily used to place satellites into low Earth and sun-synchronous orbits.

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Statements (45)

Predicate Object
instanceOf expendable launch system
orbital launch vehicle
alsoKnownAs CZ-2D NERFINISHED
Chang Zheng 2D NERFINISHED
countryOfOrigin China
designPurpose reliable access to low Earth orbit
reliable access to sun-synchronous orbit
developedBy China Aerospace Science and Technology Corporation NERFINISHED
enteredService 1990s
familyRole variant optimized for sun-synchronous missions
familyVariantOf Long March 2 NERFINISHED
firstStageEngineType YF-21C NERFINISHED
guidanceSystem inertial guidance
launchCapability low Earth orbit
sun-synchronous orbit
launchEnvironment land-based launch pad
launchMarket domestic Chinese payloads
international commercial payloads
launchProfile vertical takeoff
launchSitesUsed Jiuquan Satellite Launch Center NERFINISHED
Taiyuan Satellite Launch Center NERFINISHED
Xichang Satellite Launch Center NERFINISHED
launchVehicleType medium-lift launch vehicle
manufacturer Shanghai Academy of Spaceflight Technology NERFINISHED
missionProfile inclined low Earth orbit launches
polar orbit launches
operator China Aerospace Science and Technology Corporation NERFINISHED
China National Space Administration NERFINISHED
partOfFamily Long March rocket family NERFINISHED
primaryUse launching satellites to low Earth orbit
launching satellites to sun-synchronous orbit
propellantCombination nitrogen tetroxide
unsymmetrical dimethylhydrazine
propellantType hypergolic propellant
reusability non-reusable
rocketConfiguration two-stage
secondStageEngineType YF-24C NERFINISHED
stages 2
status operational
technologyBase Long March 2 core technology
usedBy People's Republic of China NERFINISHED
usedFor Earth observation satellites NERFINISHED
remote sensing satellites
scientific satellites
technology demonstration satellites

Referenced by (1)

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