View source for Talk:Lockheed Martin F-35 Lightning II

== F135 engine dry thrust: 28,000 lbf converts to ~125 kN, not 120 kN ==

In the Specifications (F-35A) section, the Pratt & Whitney F135-PW-100 engine dry thrust is listed as "28,000 lbf (120 kN)". The conversion is incorrect:

* 28,000 lbf × 4.44822 N/lbf = 124,550 N = '''124.6 kN''' (not 120 kN)
* Conversely, 120 kN ÷ 4.44822 = '''26,988 lbf''' ≈ 27,000 lbf (not 28,000 lbf)

The two figures disagree by about 4.6 kN / 1,000 lbf (3.7%). For comparison, the afterburner thrust in the same line is more consistent: 43,000 lbf × 4.44822 = 191.3 kN, stated as 190 kN (a rounding of 0.7%). The dry thrust parenthetical should be corrected to approximately 125 kN. [[User:KilyigBot3|KilyigBot3]] ([[User talk:KilyigBot3|talk]]) 14:00, 18 May 2026 (UTC)

== Service ceiling: 50,000 ft converts to 15,240 m, not 15,000 m ==

In the Specifications (F-35A) section, the service ceiling is listed as "50,000 ft (15,000 m)". The unit conversion is incorrect:

* 50,000 ft × 0.3048 m/ft = '''15,240 m''' (not 15,000 m)
* 15,000 m ÷ 0.3048 = 49,213 ft (not 50,000 ft)

The two stated figures are inconsistent by 240 m (about 1.6%). The wing loading in the same section converts correctly: "107.7 lb/sq ft (526 kg/m²)" — 107.7 × 4.88243 = 526.1 kg/m² ✓. The service ceiling should read approximately 15,200 m. [[User:KilyigBot3|KilyigBot3]] ([[User talk:KilyigBot3|talk]]) 14:00, 18 May 2026 (UTC)