[permalink] [id link]
| afterburning thrust main = 33. 8 kN
from
Wikipedia
Some Related Sentences
| and afterburning
| afterburning thrust main =
| afterburning thrust alt =
| type of jet = afterburning turbojets
| type of jet = afterburning turbojet
| afterburning thrust alt = 7, 423 lbf
| type of jet = afterburning turbofan
| thrust main = 72. 1 kN / 125. 0 kN afterburning
| thrust alt = 16, 200 lbf dry, 28, 110 lbf afterburning
| afterburning thrust main = 60. 80 kN
| afterburning thrust alt = 13, 668 lbf
| afterburning thrust main = 32. 5 kN
| afterburning thrust alt = 7, 305 lbf
| type of jet = afterburning turbojet
| afterburning thrust main =
| afterburning thrust alt =
| type of jet = afterburning turbojet
| thrust main = 83. 6 kN dry, 127 kN afterburning
| afterburning thrust main = 14, 750 lbf
| afterburning thrust alt = 65. 77 kN
| afterburning thrust main = 16, 000 lbf
| afterburning thrust alt = 71 kN
| type of jet = afterburning turbojet
| afterburning thrust main = 17, 200 lbf
| afterburning thrust alt = 76. 5 kN
| and thrust
Image: Parc Guell 10. jpg | Colonnaded footpath under the roadway viaduct, with external columns sloping to take the diagonal thrust from the vault supporting the road.
| thrust main = 1, 600 lbf
| thrust alt = 7. 1 kN
| thrust / weight = 0. 32
Explanations: A-fold ( geology ) | folded rock strata cut by a thrust fault ; B-large intrusion ( cutting through A ); C-erosion al angular unconformity ( cutting off A & B ) on which rock strata were deposited ; D-dike ( geology ) | volcanic dyke ( cutting through A, B & C ); E-even younger rock strata ( overlying C & D ); F-normal fault ( cutting through A, B, C & E ).
| thrust / weight =
| thrust / weight =
| thrust main = 9, 275 lb < sub > f </ sub >
| thrust alt = 41. 26 kN
| thrust / weight = 0. 353
A 1596 sketch of a rehearsal in progress on the thrust stage of The Swan ( theatre ) | The Swan, a typical circular Elizabethan open-roof playhouse.
| thrust main = 54. 09 kN
| thrust alt = 12, 160 lbf
| thrust / weight =
| thrust main = 3, 500 lbf
| thrust alt = 15. 6 kN
| thrust / weight = 0. 45
| thrust main = 11, 000 lbf
| thrust alt = 49 kN
| thrust original =
| thrust / weight = 0. 31
| thrust main = 31. 9 kN
0.070 seconds.