Jun 032010
Similar to the L-6 previously described, but with hydrogen for fuel rather than RP-1. Chamber pressure, 1000 psia; 6,000,000 lbs thrust; 359 seconds Isp sea level, 416 seconds vacuum.
Sadly, the quality of the reproduction of the drawing is utter crap. Virtually nothing legible.
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[…] L-24 AH used four of the turbopumps used by the individual 6-million pound thrust L-6H hydrogen/oxygen engines. Chamber pressure was 2000 psi and the expansion ratio was 40. This engine used a toroidal […]