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 |
|---|---|
| RD-93 | around 81–85 kN with afterburner ⓘ |
| SMR-95 | medium ⓘ |
|
Whittle W.1 turbojet engine
surface form:
Whittle W.1
|
around 860 lbf ⓘ |
| F118 | approximately 17,000 lbf ⓘ |
| JT3C | high-thrust ⓘ |
| Pratt & Whitney J75 | 75–80 kN dry ⓘ |
| Pratt & Whitney J75 | 110–120 kN with afterburner ⓘ |
| Rolls-Royce BR725 A1-12 | approximately 16000 lbf ⓘ |
| F110 | approximately 28,000–32,000 lbf with afterburner ⓘ |
| Lyulka AL-31F | approximately 75 kN dry ⓘ |
| Lyulka AL-31F | approximately 122–125 kN with afterburner ⓘ |
| MTR390 | 1,000–1,500 shp class via predicate surface "thrustCategory" ⓘ |
| General Electric YF120 | approximately 35,000 lbf class in afterburner ⓘ |
| General Electric YF120 | approximately 24,000–26,000 lbf class dry ⓘ |
| RB199 | around 40 kN dry ⓘ |
| RB199 | around 70–80 kN with afterburner ⓘ |
| RB199-34R Mk 101 | around 40 kN dry ⓘ |
| RB199-34R Mk 101 | around 70 kN with afterburner ⓘ |
| F119 | approximately 35000 lbf dry ⓘ |
| F119 | over 35000 lbf with afterburner ⓘ |
|
PW5000 (development designation)
surface form:
PW5000
|
high-thrust military turbofan ⓘ |
| Rolls-Royce Turbomeca F405-RR-401 | low-bypass turbofan ⓘ |
| Safran Arriel 1 series | shaft power below 1,000 kW class via predicate surface "thrustCategory" ⓘ |
| JT3D | approximately 16,000–21,000 lbf ⓘ |
| TF33 | approximately 17,000 lbf to 21,000 lbf ⓘ |
|
Armstrong Siddeley Sapphire (turbojet engine)
surface form:
Armstrong Siddeley Sapphire
|
7000–11000 lbf ⓘ |
|
Armstrong Siddeley Viper (turbojet engine)
surface form:
Armstrong Siddeley Viper
|
approximately 1,500–3,000 lbf ⓘ |
|
WS-10 Taihang turbofan
surface form:
WS-10 Taihang
|
approximately 120 kN with afterburner ⓘ |
|
WS-10 Taihang turbofan
surface form:
WS-10 Taihang
|
approximately 75–80 kN dry ⓘ |
| Rolls-Royce AE family | medium thrust ⓘ |
| Olympus 593 | high-thrust ⓘ |
| Olympus 104 | medium-to-high thrust military turbojet ⓘ |
| Olympus 301 | high thrust ⓘ |
| Soloviev D-30F6 | high-thrust military turbofan ⓘ |
| SNECMA Atar 9B | around 6000 kgf dry ⓘ |
| SNECMA Atar 9B | around 9000 kgf with afterburner ⓘ |
| Pratt & Whitney Canada PW300 series | medium-thrust ⓘ |
| WS-10 | approximately 120 kN with afterburner ⓘ |
| WS-10 | approximately 75–80 kN dry ⓘ |
| WS-15 | high thrust ⓘ |
| AJ-60 series | approximately 1.6 MN at sea level (AJ-60A) ⓘ |
| General Electric CF34-8E | approximately 14,000–15,000 lbf ⓘ |
| Ivchenko-Progress D-18T | over 200 kN ⓘ |
|
Rolls-Royce Derwent turbojet
surface form:
Rolls-Royce Derwent
|
around 2,000 lbf to 3,600 lbf depending on variant ⓘ |
| Turbomeca Marboré | around 3.9 kN to 4.0 kN ⓘ |
| JT11D-20 | high-thrust military turbojet ⓘ |
| Garrett TFE731 turbofan | small turbofan ⓘ |
| General Electric J35 | early turbojet thrust range (on the order of several thousand pounds-force) ⓘ |
| General Electric J73 | higher thrust than earlier U.S. turbojets ⓘ |
|
Rolls-Royce Viper turbojet
surface form:
Rolls-Royce Viper
|
approximately 7–18 kN depending on variant ⓘ |