launchMass
P7196
predicate
Indicates the total mass of an object or payload at the moment it is launched.
All labels observed (10)
| Label | Occurrences |
|---|---|
| launchMass canonical | 192 |
| massAtLaunch | 101 |
| launchWeight | 18 |
| launchMassApproximate | 6 |
| launchMassApprox | 3 |
| launchMass_kg | 2 |
| launchMassCapability | 1 |
| launchMassInformation | 1 |
| launchMassRange | 1 |
| launchMass_approx | 1 |
Description generation (PDg)
The one-sentence description above was generated by prompting gpt-5.1 with the predicate name and this instruction.
Instruction
Given a predicate that represents a relationship or action between entities, generate a one-sentence description explaining its meaning. # Instructions Focus on describing the relationship, not the entities themselves. # Response Format Begin the description with \' Indicates...\'
Input
Predicate: launchMass
Generated description
Indicates the total mass of an object or payload at the moment it is launched.
Sample triples (326)
| Subject | Object |
|---|---|
| Tianhe core module | about 22,500 kilograms ⓘ |
| Atlantis | about 2,030,000 kg with external tank and boosters ⓘ |
| Inertial Upper Stage | approximately 14,000 kilograms ⓘ |
|
UR-100 ICBM
surface form:
UR-100
|
about 41,000 kg via predicate surface "launchWeight" ⓘ |
| Delta IV Heavy | 733000 kg ⓘ |
| InSight Mars lander | about 694 kg via predicate surface "massAtLaunch" ⓘ |
| Vostok 5 | 4725 kg ⓘ |
| Compton Gamma Ray Observatory | 17000 kilograms via predicate surface "massAtLaunch" ⓘ |
| STS-51-C | about 115000 kg ⓘ |
| Apollo 9 | about 45,000 kg for the Command and Service Module ⓘ |
| GSAT-19 | 3136 kg ⓘ |
| Pegasus micrometeoroid satellites | approximately 10,000 kilograms per spacecraft ⓘ |
| Columbus laboratory | about 12400 kg ⓘ |
| STRaND-1 | approximately 4.3 kilograms ⓘ |
|
CH-1
surface form:
Chandrayaan-1
|
1380 kg via predicate surface "massAtLaunch" ⓘ |
| IRS-1A | approximately 975 kilograms ⓘ |
| IRS-1B | approximately 975 kg ⓘ |
| Oceansat-2 | approximately 960 kg ⓘ |
|
MOM
surface form:
Mangalyaan
|
approximately 1337 kg via predicate surface "massAtLaunch" ⓘ |
| PSLV-C11 | 320000 kg via predicate surface "launchMassApproximate" ⓘ |
| INSAT-1B | about 1150 kg ⓘ |
| IRS-1D | ~1250 kg ⓘ |
| IRS-P4 | 1050 kg ⓘ |
| INSAT-1D | about 1190 kilograms ⓘ |
| Hubble Space Telescope Servicing Mission 3B | approximately 115000 kg ⓘ |
| STS-92 | about 120,000 kg ⓘ |
| STS-41 | about 117000 kg ⓘ |
| INSAT-2A | approximately 1900 kg ⓘ |
| Mariner 2 | approximately 203 kilograms via predicate surface "massAtLaunch" ⓘ |
| Surveyor 1 | 995 kilograms via predicate surface "massAtLaunch" ⓘ |
| Titan II ICBM | approximately 150,000 kilograms ⓘ |
| INSAT-2E | 2550 kilograms ⓘ |
| SpaceX COTS Demo Flight 1 | approximately 6,000 kg ⓘ |
| INSAT-3D | 2060 kg via predicate surface "massAtLaunch" ⓘ |
|
Rosetta (on earlier Ariane 5 variant family)
surface form:
Rosetta
|
about 3000 kilograms ⓘ |
| Vega | ~137000 kg ⓘ |
| Ariane 5 G | approximately 746000 kg ⓘ |
| Euclid spacecraft | approximately 2,000 kg via predicate surface "massAtLaunch" ⓘ |
| INSAT-4A | approximately 3081 kg ⓘ |
| INSAT-4B | approximately 3025 kg ⓘ |
| INSAT-4CR | approximately 2130 kilograms ⓘ |
| R-1 missile | 13,400 kg via predicate surface "launchWeight" ⓘ |
| R-2 missile | approximately 20,000 kg ⓘ |
| Pioneer 0 | approximately 38 kg ⓘ |
| Pioneer 2 | approximately 39 kilograms ⓘ |
| R-5 missile | approximately 29,000 kg ⓘ |
| INSAT-3DR | about 2211 kg ⓘ |
| Salyut 1 | 18000 kilograms (approximate) via predicate surface "massAtLaunch" ⓘ |
| Pioneer 5 | approximately 43 kg via predicate surface "massAtLaunch" ⓘ |
| Voskhod launch vehicle | ~287000 kg ⓘ |