Template talk:Engine thrust to weight table

The Thrust-to-weight ratios for the J58 and F119 are wrong according to the data.

J58: 34000/6001 = 5.7 and not 5.2 as stated.

F119: 20500/3900 = 5.3 and not 7.95 as stated.

It is easy to change the t/w value to be consistent, but since it could be any of the three values (thrust, weight or thrust/weight) that are wrong, it is unclear which correction to make. I have left it wrong to at least show that the source data is suspect.

146.90.210.170 (talk) 11:42, 15 March 2014 (UTC)