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 |
|---|---|
| Adour Mk 101 | around 5,000–6,000 lbf dry (approximate) ⓘ |
| Adour Mk 101 | around 7,000–8,000 lbf with afterburner (approximate) ⓘ |
| Adour Mk 106 | medium thrust ⓘ |
| Adour Mk 102 | approximately 5000–6000 kgf ⓘ |
| Adour Mk 107 | higher thrust than earlier Adour variants ⓘ |
| Adour Mk 104 | approximately 24 kN dry ⓘ |
| Adour Mk 104 | approximately 37 kN with afterburner ⓘ |
| Adour Mk 811 | approximately 26 kN dry ⓘ |
| Adour Mk 811 | approximately 37 kN with afterburner ⓘ |
| RM12 | 80 kN with afterburner ⓘ |
| F404-GE-100 | approximately 48 kN dry ⓘ |
| F404-GE-100 | approximately 78 kN with afterburner ⓘ |
| Adour Mk 951 | approximately 29 kN dry ⓘ |
| Adour Mk 951 | approximately 26–30 kN class ⓘ |
|
F401 (military derivative context)
surface form:
F401
|
medium thrust ⓘ |
| F124 | approximately 6,000 lbf ⓘ |
| PW2037 | approximately 37,000 lbf ⓘ |
| PW2037 | about 165 kN ⓘ |
| PW2040 | about 40,000 lbf ⓘ |
| PW2033 | medium-to-high thrust class ⓘ |
| Aviadvigatel PS-90A | 140 kN ⓘ |
| BE-4 | 2.4 MN class ⓘ |
| CFM International LEAP-1B | approximately 23,000 to 29,000 lbf ⓘ |
|
Rolls-Royce Tay (turbofan family, conceptually)
surface form:
Rolls-Royce Tay
|
approximately 13,000–15,000 lbf ⓘ |
| Pratt & Whitney JT3C | 11000–13000 lbf ⓘ |
| Rolls-Royce Pearl 15 | 15000 lbf ⓘ |
| Rolls-Royce Pearl 15 | approximately 67 kN ⓘ |
| CF6-6 | lower-thrust variant ⓘ |
| CF6-80A | approximately 48,000 lbf to 52,000 lbf ⓘ |
| Rolls-Royce AE 3007H | approximately 7,000–8,000 lbf ⓘ |
| Klimov RD-45 | around 22 kN dry thrust ⓘ |
| Rolls-Royce Derwent | around 2,000 lbf to 3,600 lbf depending on variant ⓘ |
| Pratt & Whitney J42 | approximately 5000 lbf ⓘ |
| CF6-50 | higher-thrust variant of CF6 ⓘ |
| CF6-80C2 | approximately 52,000 to 61,500 lbf ⓘ |
| General Electric GE90 | 81,000–115,000 lbf ⓘ |
|
Pratt & Whitney TF30 afterburning turbofan
surface form:
Pratt & Whitney TF30
|
approximately 20,000 lbf with afterburner ⓘ |
|
Pratt & Whitney TF30 afterburning turbofan
surface form:
Pratt & Whitney TF30
|
approximately 12,000 lbf dry ⓘ |
| Rolls-Royce Trent 500 | very high thrust ⓘ |
| Rolls-Royce Pearl 700 | approximately 18,000 lbf ⓘ |
| Armstrong Siddeley Sapphire | around 7,000–11,000 lbf depending on variant ⓘ |
| Rolls-Royce Adour | approximately 5,000–6,500 lbf dry ⓘ |
| Rolls-Royce Adour | over 8,000 lbf with afterburner (reheat) in some variants ⓘ |
| Ivchenko AI-25 | approximately 14 kN to 17 kN ⓘ |
| Rolls-Royce Trent 800 | 80,000 lbf ⓘ |
| Pratt & Whitney TF33 | approximately 17,000 to 21,000 pounds-force ⓘ |
| General Electric J79 | approximately 10,000–18,000 pounds-force with afterburner depending on variant ⓘ |
| Rolls-Royce BR715 | 18000–21500 lbf ⓘ |
| RD-33 Series 2 | medium thrust ⓘ |
| RD-93 | around 49 kN dry ⓘ |