Talk:F-11 Tiger
From Wikipedia, the free encyclopedia
 |
F-11 Tiger is part of WikiProject Aircraft, an attempt to better organize articles related to aircraft. If you would like to participate, you can edit the article attached to this page or visit the project page where you can join the project and/or contribute to the discussion. |
| ??? | This article has not yet received a rating on the quality scale. Please rate the article and then leave a short summary here to explain the ratings and/or to identify the strengths and weaknesses of the article. |
| ??? | This article has not yet received a rating on the importance scale. |
|
|
|
[edit] Specifications
Initial rate of climb appears wrong, although I do not have a reference. Compare it to its subsonic peers with lower thrust/weight (e.g., F-86 / FJ Fury models). With a thrust to weight of almost .5 to 1, and transsonic capability from MSL to its service ceiling, it should climb in excess of 10,000 fpm. Joe Baugher and Global Security cite the same figure. Anybody have another data source? Or is the climb figure based on max T/O weight instead of the usual air-to-air loadout plus 60% fuel? --RandallC 09:33, 12 July 2006 (UTC)
