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NK-9V-11D53
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Manufacturer Name: NK-9V-11D53. Government Designation: 11D53. Other Designations: NK-21. Designer: Kuznetsov. Application: N-1 stage 3 (block V). Propellants: Lox/Kerosene. Thrust(vac): 449.000 kN (100,939 lbf). Isp: 340 sec. Isp (sea level): 312 sec. Chambers: 1. Country: Russia. Status: Out of Production. Modification of NK-9 engine for the N-1 lunar rocket. May be identical to NK-21 (stage 3).
Bibliography and Further Reading - Kobelyev, V N; Milovanov, A G, Rakety Nositeli, Moscow State Aviation Techology University, 1993 via Dietrich Haeseler.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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