massToLowEarthOrbit
P84008
predicate
Indicates the amount of mass that can be transported by a launch system into low Earth orbit.
Observed surface forms (7)
| Surface form | Occurrences |
|---|---|
| typicalPayloadMassToLEO | 3 |
| geocentricOrbitPayloadCapacity | 1 |
| launchCapabilityToLEO | 1 |
| launchMassToOrbit_kg | 1 |
| launchMassTotalPayload | 1 |
| launchToLEO | 1 |
| massToOrbitComparedTo | 1 |
Sample triples (10)
| Subject | Object |
|---|---|
| LauncherOne | approximately 300 kg ⓘ |
| LVM3 | approximately 8 tonnes via predicate surface "launchCapabilityToLEO" ⓘ |
| Pegasus XL | approximately 443 kg via predicate surface "typicalPayloadMassToLEO" ⓘ |
| New Glenn | heavy-lift class capability via predicate surface "launchToLEO" ⓘ |
|
taller than SLS Block 1
surface form:
Space Launch System Block 1B
|
greater than SLS Block 1 via predicate surface "massToOrbitComparedTo" ⓘ |
| H-2B | low Earth orbit via predicate surface "geocentricOrbitPayloadCapacity" ⓘ |
| Pegasus rocket family | around 400 kg via predicate surface "typicalPayloadMassToLEO" ⓘ |
| Electron | approximately 300 kg via predicate surface "typicalPayloadMassToLEO" ⓘ |
| PSLV-C2 | ~1050 via predicate surface "launchMassToOrbit_kg" ⓘ |
| PSLV-C14 | ~1000 kg via predicate surface "launchMassTotalPayload" ⓘ |