thrustClass
P17733
predicate
Indicates the classification of an engine or propulsion system based on the amount or category of thrust it can produce.
All labels observed (3)
| Label | Occurrences |
|---|---|
| thrustClass canonical | 201 |
| thrustCategory | 3 |
| thrustComparedToBlock1 | 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: thrustClass
Generated description
Indicates the classification of an engine or propulsion system based on the amount or category of thrust it can produce.
Sample triples (205)
| Subject | Object |
|---|---|
| Engine Alliance GP7200 | around 70,000 lbf to 81,000 lbf ⓘ |
| PW4000 series | 52,000–99,000 lbf ⓘ |
| Rolls-Royce Trent XWB | 70000–97000 lbf ⓘ |
| Pratt & Whitney PW1500G | 14000–24000 lbf ⓘ |
| Falcon 9 first stage booster B1064 | Falcon 9 first stage thrust class ⓘ |
| Rolls-Royce/Snecma Olympus 593 | around 38,000 lbf dry ⓘ |
| Rolls-Royce/Snecma Olympus 593 | around 38,000–40,000 lbf with reheat ⓘ |
| F117 | high-thrust military transport engine ⓘ |
| Pratt & Whitney JT3D | approximately 17,000 lbf to 21,000 lbf ⓘ |
| AE 3007A | approximately 7,000 to 8,000 pounds-force ⓘ |
| Rolls-Royce AE 3007A1/3 | regional jet engine ⓘ |
| IAE V2500 | 22000–33000 lbf ⓘ |
| Pratt & Whitney Canada PW307A | medium thrust business jet engine ⓘ |
| General Electric J47 | approximately 5,000 to 6,000 pounds-force dry ⓘ |
| Garrett TFE731-2 | approximately 3500 lbf ⓘ |
|
Mikulin AM-3 turbojet
surface form:
Mikulin AM-3
|
high-thrust turbojet ⓘ |
| Pratt & Whitney PW6000 | medium thrust turbofan via predicate surface "thrustCategory" ⓘ |
| R-1 missile | similar to V-2 rocket ⓘ |
| CFM International CFM56-5B | 22000–33000 lbf ⓘ |
|
Kolesov RD-36-51 turbojet engine
surface form:
Kolesov RD-36-51
|
high thrust ⓘ |
|
Rolls‑Royce Welland
surface form:
Rolls-Royce Welland
|
about 7 kN ⓘ |
|
Volvo RM9 turbojet
surface form:
Volvo RM9
|
low-thrust turbojet ⓘ |
| Argus As 014 | approximately 2.7–3.0 kN ⓘ |
| Argus As 014 | approximately 660–700 lbf ⓘ |
| Snecma M88 | medium thrust ⓘ |
| Saturn AL-31F | approximately 75 kN dry ⓘ |
| Saturn AL-31F | approximately 122 kN with afterburner ⓘ |
|
Rolls-Royce Spey turbofan
surface form:
Rolls-Royce Spey
|
9000 to 12000 lbf (civil versions) ⓘ |
|
Rolls-Royce Spey turbofan
surface form:
Rolls-Royce Spey
|
up to about 20000 lbf (military afterburning versions) ⓘ |
| General Electric TF39 | around 40,000 lbf ⓘ |
| General Electric TF39 | approximately 178 kN ⓘ |
| Volvo RM8 | high subsonic to supersonic with afterburner ⓘ |
| Rolls-Royce Viper | approximately 1,500–4,000 lbf ⓘ |
| GE Honda HF120 | about 2000 lbf ⓘ |
| GE Honda HF120 | around 8.9 kN ⓘ |
| Rolls-Royce Trent family | high-thrust ⓘ |
| Rolls-Royce AE 2100 | medium-power turboprop ⓘ |
|
Allison 501 civil engine family
surface form:
Allison 501
|
shaft power class up to several thousand shp ⓘ |
| RocketMotorOne | approximately 80 kN ⓘ |
| Pratt & Whitney Canada PW308A | 6800 lbf ⓘ |
| Pratt & Whitney Canada PW308A | approximately 30 kN ⓘ |
| General Electric J85 | around 2,950 lbf dry ⓘ |
| General Electric J85 | around 4,300–5,000 lbf with afterburner (depending on variant) ⓘ |
|
Williams FJ44-2 turbofan
surface form:
Williams FJ44-2
|
small turbofan thrust class ⓘ |
| CF6-80E1A3 | high thrust ⓘ |
| Rolls-Royce RB.168 | approximately 20,000 lbf ⓘ |
| Bristol Orpheus | around 4,000 lbf ⓘ |
| Bristol Orpheus | around 18 kN ⓘ |
| Pegasus 11 | higher than earlier Pegasus variants ⓘ |
| PowerJet SaM146 | 68–79 kN ⓘ |