thrust
P14228
predicate
Indicates a forceful forward push or drive exerted by one entity onto another or into a particular direction.
All labels observed (7)
| Label | Occurrences |
|---|---|
| thrustVacuum | 48 |
| thrust canonical | 18 |
| overthrusts | 7 |
| engineThrust | 6 |
| thrustWithAfterburner | 6 |
| thrustDry | 5 |
| providesThrust | 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: thrust
Generated description
Indicates a forceful forward push or drive exerted by one entity onto another or into a particular direction.
Sample triples (91)
| Subject | Object |
|---|---|
| V-2 rocket | approximately 25 metric tons ⓘ |
| Eurojet EJ200 | 6000 kgf via predicate surface "thrustDry" ⓘ |
| Eurojet EJ200 | about 60 kN via predicate surface "thrustDry" ⓘ |
| Eurojet EJ200 | 9000 kgf via predicate surface "thrustWithAfterburner" ⓘ |
| Eurojet EJ200 | about 90 kN via predicate surface "thrustWithAfterburner" ⓘ |
| Merlin 1A | about 340 kN via predicate surface "thrustVacuum" ⓘ |
| North American X-15 | 254000 newtons via predicate surface "engineThrust" ⓘ |
| North American X-15 | 57000 pounds-force via predicate surface "engineThrust" ⓘ |
| RL10 | approximately 110 kN via predicate surface "thrustVacuum" ⓘ |
| Draco thrusters | about 400 newtons via predicate surface "thrustVacuum" ⓘ |
| Draco thrusters | about 90 pounds-force via predicate surface "thrustVacuum" ⓘ |
| Aggregat 4 | about 25 metric tons at liftoff ⓘ |
| R-1 rocket | approximately 270 kN ⓘ |
| Interim Cryogenic Propulsion Stage | approximately 110 kN via predicate surface "thrustVacuum" ⓘ |
|
Rolls-Royce LiftSystem
linked to:
Rolls-Royce LiftSystem (F-35B integration)
|
vertical lift thrust via predicate surface "providesThrust" ⓘ |
|
Junkers Jumo 004
linked to:
Junkers Jumo 004 turbojet engine
|
approximately 8.8 kN ⓘ |
|
Junkers Jumo 004
linked to:
Junkers Jumo 004 turbojet engine
|
approximately 1,980 lbf ⓘ |
| SpaceShipOne | approximately 75 kN ⓘ |
| Reaction Motors XLR11 | about 6,000 pounds-force via predicate surface "thrustVacuum" ⓘ |
| Reaction Motors XLR11 | about 27 kilonewtons via predicate surface "thrustVacuum" ⓘ |
| Reaction Motors XLR99 | about 57,000 lbf via predicate surface "thrustVacuum" ⓘ |
| Reaction Motors XLR99 | about 254 kN via predicate surface "thrustVacuum" ⓘ |
| General Electric F414-GE-400 | approximately 14,000 lbf via predicate surface "thrustDry" ⓘ |
| S-IVB | about 1,033 kN via predicate surface "thrustVacuum" ⓘ |
| S-IVB | about 232,000 lbf via predicate surface "thrustVacuum" ⓘ |
| J-2 | approximately 1,033 kN via predicate surface "thrustVacuum" ⓘ |
| J-2 | approximately 232,000 lbf via predicate surface "thrustVacuum" ⓘ |
| LR-91 | approximately 444 kilonewtons via predicate surface "thrustVacuum" ⓘ |
| LR-91 | approximately 100,000 pounds-force via predicate surface "thrustVacuum" ⓘ |
| Heinkel He 178 | approximately 4.9 kN via predicate surface "engineThrust" ⓘ |
| Heinkel He 178 | approximately 1,100 lbf via predicate surface "engineThrust" ⓘ |
| MiG-35 | approximately 9,000 kgf per engine via predicate surface "thrustWithAfterburner" ⓘ |
|
Lyulka AL-21F-3
linked to:
Lyulka AL-21F-3 turbojet
|
approximately 76 kN via predicate surface "thrustDry" ⓘ |
|
Lyulka AL-21F-3
linked to:
Lyulka AL-21F-3 turbojet
|
approximately 110 kN via predicate surface "thrustWithAfterburner" ⓘ |
| Manned Maneuvering Unit | approximately 24 newtons per thruster ⓘ |
| RS-25D | about 2.3 meganewtons via predicate surface "thrustVacuum" ⓘ |
| Main Central Thrust zone | Lesser Himalayan rocks via predicate surface "overthrusts" ⓘ |
| Main Boundary Thrust zone | Lesser Himalayan rocks onto Siwalik rocks via predicate surface "overthrusts" ⓘ |
| Orbital Maneuvering System | about 26.7 kilonewtons per engine via predicate surface "thrustVacuum" ⓘ |
| Pratt & Whitney J58 | approximately 32,500 lbf via predicate surface "thrustDry" ⓘ |
| Pratt & Whitney J58 | approximately 34,000 lbf via predicate surface "thrustWithAfterburner" ⓘ |
| Pratt & Whitney J58 | approximately 145 kN via predicate surface "thrustWithAfterburner" ⓘ |
| Rocketdyne H-1 | about 205,000 lbf via predicate surface "thrustVacuum" ⓘ |
| Rocketdyne H-1 | about 912 kN via predicate surface "thrustVacuum" ⓘ |
| Klimov VK-1 | about 26.5 kN dry ⓘ |
| Klimov VK-1 | about 5,950 lbf dry ⓘ |
| Vulcain 2 | approximately 1350 kN via predicate surface "thrustVacuum" ⓘ |
| HM7B | 62 kN via predicate surface "thrustVacuum" ⓘ |
| R-2 missile | greater than V-2 rocket thrust ⓘ |
|
RS-68
linked to:
RS-68 engine
|
about 3,137 kN via predicate surface "thrustVacuum" ⓘ |