The LEO and GTO inclinations are a bit different too on the page...
Falcon 9 v1.2+ 2016 est 5/2/2016 Masses and Forces in Metric Tons (Tonnes), Velocity in Meters/Second PMF GLOW Mpusuable Mfinal Thrust Isp0.96 Stage 1 424.6237338 407.6387844 16.98494935 775 3020.96 Stage 2 111.7 107.232 4.468 95 348 Fairing 2.0 Payload 8.3 Mi Mf Delta-v Burn Time T/W GLOW-PL Flight Stg 1 546.6237338 138.9849494 4054.929359 158.8476295 1.417794274 536.3237338 Flight Stg 2 120 12.768 7645.06926 392.8077474 0.791666667 Total 11699.99862
For reference, Falcon91.0 second stage was 2957 kghttp://forum.nasaspaceflight.com/index.php?topic=28882.msg915790#msg915790Assuming:!450 kg domes (Al-Li 12 mm thick)600 kg side skin (Al-Li 5 mm thick)700 kg engine200 kg othersFalcon9 1.1 second stage could be1450 kg domes (same as v1.0)1300 kg side skin (more than double)700 kg engine (same as v1.0)350 kg others (some more helium)3800 kgFor Falcon FT lenght is 20% more (and helium must be more) therefore something like 4100-4200 kg
In June 2015 Tom Mueller answered a question about the Merlin 1D thrust-weight ratios on Quora. He specified that the Merlin 1D has a weight of 1,030 lb (470 kg) including thrust actuators, a current vacuum thrust of 162,500 pounds-force (723 kN), and an uprated vacuum thrust of 185,500 pounds-force (825 kN), which still weighs the same.
Anybody have a firmer figure for mass of Merlin 1D FT vacuum? Cambrianera estimates 700 kg for that. 1D FT regular version masses 470 kg.