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The N1 was a very large rocket, standing 105 meters (344 ft) tall with its L3 payload. The N1-L3 consisted of five stages in total: the first three (N1) for insertion into a low Earth parking orbit, and another two (L3) for translunar injection and lunar orbit insertion. Fully loaded and fueled, the N1-L3 weighed 2,750 tonnes (6,060,000 lb). The lower three stages were shaped to produce a single frustum 17 meters (56 feet) wide at the base,[8] while the L3 section was mostly cylindrical, carried inside a shroud 3.5 meters (11 feet) (estimated) wide.[9] The conical shaping of the lower stages was due to the arrangement of the tanks within, a smaller spherical kerosene tank on top of the larger liquid oxygen tank below.
The first stage, Block A, was powered by 30 NK-15 engines arranged in two rings, the main ring of 24 at the outer edge of the booster and the core propulsion system consisting of the inner 6 engines at about half diameter.[10] The engines were the first ever staged combustion cycle engines. The control system was primarily based on differential throttling of the engines of the outer ring for pitch and yaw. The core propulsion system was not used for control.[11] The Block A also included four grid fins, which were later used on Soviet air-to-air missile designs. In total, the Block A produced 45,400 kN (10,200,000 lbf)[12][13][14] of thrust. This exceeded the 33,700 kN (7,600,000 lbf) thrust of the Saturn V.[15] The Saturn V used higher-specific impulse liquid hydrogen fuel in the second and third stages, which eliminated one of the stages needed to get to translunar injection, thus saving weight.
Yeah, like that worked for China, didn't it?
I mean, shure. I beats war / pestilence...