Long March 4B
E714660
Long March 4B is a Chinese three-stage orbital launch vehicle used primarily to place satellites into sun-synchronous and low Earth orbits.
Statements (39)
| Predicate | Object |
|---|---|
| instanceOf |
expendable launch system
ⓘ
orbital launch vehicle ⓘ |
| alsoKnownAs | Chang Zheng 4B NERFINISHED ⓘ |
| countryOfOrigin | China ⓘ |
| designPurpose | high-inclination orbits ⓘ |
| familyDesignation | CZ-4B NERFINISHED ⓘ |
| hasVariant | Long March 4C NERFINISHED ⓘ |
| launchCapability |
polar orbit
ⓘ
sun-synchronous orbit ⓘ |
| launchEnvironment | land-based launch pad ⓘ |
| launchMarket |
commercial payloads
ⓘ
government payloads ⓘ |
| launchProfile | vertical takeoff ⓘ |
| launchRole | medium-lift launcher ⓘ |
| launchSitesUsed |
Jiuquan Satellite Launch Center
NERFINISHED
ⓘ
Taiyuan Satellite Launch Center NERFINISHED ⓘ Xichang Satellite Launch Center NERFINISHED ⓘ |
| manufacturer |
China Academy of Launch Vehicle Technology
NERFINISHED
ⓘ
Shanghai Academy of Spaceflight Technology NERFINISHED ⓘ |
| operator |
China National Space Administration
NERFINISHED
ⓘ
People's Republic of China NERFINISHED ⓘ |
| partOfFamily | Long March rocket family NERFINISHED ⓘ |
| primaryMissionType | satellite launch ⓘ |
| propellantTypeFirstStage | N2O4/UDMH ⓘ |
| propellantTypeSecondStage | N2O4/UDMH ⓘ |
| propellantTypeThirdStage | N2O4/UDMH ⓘ |
| propulsionType | liquid-fueled ⓘ |
| reusability | non-reusable ⓘ |
| rocketConfiguration | three-stage ⓘ |
| staging | three-stage to orbit ⓘ |
| status | operational ⓘ |
| successorTo | Long March 4A NERFINISHED ⓘ |
| typicalInclination | high-inclination orbits ⓘ |
| typicalOrbit |
low Earth orbit
ⓘ
sun-synchronous orbit ⓘ |
| usedFor |
Earth observation satellites
ⓘ
meteorological satellites ⓘ remote sensing satellites ⓘ scientific satellites ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.