thrust
1,686
triples
GPTKB property
Alternative names (8)
afterburner
•
thrust class
•
thrustClass
•
thrustDry
•
thrustPerEngine
•
thrustRange
•
thrustWithAfterburner
•
thrustWithoutAfterburner
Random triples
| Subject |
Object |
|
gptkb:Pratt_&_Whitney_JT3D
|
18,000 lbf
|
|
gptkb:SNECMA_Atar_9C_turbojet
|
6,000 kgf (13,230 lbf)
|
|
gptkb:Minuteman_missile_engines
|
second stage: ~60,000 lbf
|
|
gptkb:de_Havilland_Ghost_turbojet
|
5,000 lbf
|
|
gptkb:ELA-3
|
67 kN
|
|
gptkb:Antares_first_stage
|
3,265 kN
|
|
gptkb:CF34_family
|
8,729 to 20,360 lbf
|
|
gptkb:Delta_IV_second_stage
|
110 kN
|
|
gptkb:PW545B
|
4,119 lbf
|
|
gptkb:Harrier_jump_jet_engine_(Pegasus)
|
21,750 lbf (Pegasus 11-61)
|
|
gptkb:Allison_J33-A-35
|
4,600 lbf
|
|
gptkb:Apollo_Lunar_Module_descent_engine_system
|
10,125 lbf
|
|
gptkb:Titan_IIIB
|
1,900 kN (first stage)
|
|
gptkb:Rolls-Royce_Trent_500
|
53,000–60,000 lbf
|
|
gptkb:de_Havilland_Gyron_Junior
|
8,000 lbf dry
|
|
gptkb:Redstone_rocket_family
|
350 kN (PGM-11 Redstone)
|
|
gptkb:General_Electric_J85-GE-21B
|
2,950 lbf (13.1 kN)
|
|
gptkb:IHI_J85_engine
|
2,200 lbf
|
|
gptkb:IHI_J74_engine
|
3,300 lbf
|
|
gptkb:F135_engine
|
43,000 lbf (with afterburner)
|