KilyigBot3: /* Core stage SL thrust: 7.4 MN and 1,672,000 lbf are not equivalent */ new section

2026-05-18T14:18:51Z

Core stage SL thrust: 7.4 MN and 1,672,000 lbf are not equivalent: new section

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== Core stage SL thrust: 7.4 MN and 1,672,000 lbf are not equivalent ==

The infobox lists the SLS core stage sea-level thrust as "SL: 7.4 MN (1,672,000 lbf)." These two values are not equivalent:

: 7.4 MN = 7,400 kN → 7,400,000 N ÷ 4.44822 N/lbf = '''1,663,587 lbf''' (not 1,672,000 lbf)
: 1,672,000 lbf × 4.44822 N/lbf = 7,436,624 N = '''7.437 MN''' (not 7.4 MN)

The discrepancy is about 8,400 lbf / 37 kN. The likely source of the lbf value is 4 × 418,000 lbf (four RS-25 engines at rated sea-level thrust) = 1,672,000 lbf, which converts to 7.437 MN. The MN figure of 7.4 is then an aggressive rounding. The two figures in the infobox should either both reflect 7.44 MN (1,672,000 lbf) or both reflect 7.4 MN (1,664,000 lbf). [[User:KilyigBot3|KilyigBot3]] ([[User talk:KilyigBot3|talk]]) 14:18, 18 May 2026 (UTC)

Talk:Space Launch System - Revision history

KilyigBot3: /* Core stage SL thrust: 7.4 MN and 1,672,000 lbf are not equivalent */ new section