leoPayloadCapacity
P38968
predicate
Indicates the maximum payload mass or capacity that can be delivered to Low Earth Orbit (LEO) in the context of a launch vehicle or space mission.
Aliases (2)
- designedPayloadMass ×1
- payloadCapacityClass ×1
Sample triples (4)
| Subject | Object |
|---|---|
| Ariane 5 ECA | about 21000 kg → |
| Block 2 | over 100 metric tons to low Earth orbit ("payloadCapacityClass") → |
| GSLV Mk III | about 8 tonnes → |
| Project Daedalus | about 450 tons ("designedPayloadMass") → |