The NK-33 was an improved version of the earlier NK-15 engine, which powered the original N1 launch vehicle. Key upgrades included simplified pneumatic and hydraulic systems, advanced …

nk-33和nk-43是苏联60年末70年代初由库兹涅佐夫设计局设计制造的火箭发动机。 用于登月火箭 N1 。 NK-33的 推重比 是当前比冲最高的火箭发动机之一。

nk-33是从n1火箭项目的nk-15煤油发动机发展而来的，推力约1500 kn左右，采用了富氧燃烧和分级补燃技术，推重比133.7：1。 [1] NK-33发动机的设计实现了较高的性能和很轻的结构重量。

NK-33和NK-43是苏联60年末70年代初由库兹涅佐夫设计局设计制造的火箭发动机，用于登月火箭N1。NK-33的推重比曾经是发动机领域最高的，现已被Merlin1D大幅超越，2014年版本 …

NK—33发动机的结构牢固可靠,可实现很高的泵出口压力和14.480MPa 绝压的高燃烧室压力,因此,其面积比可达27:1,可产生2913.57m/s 的海平面比冲和3274.1m/s 的真空比冲。

nk-33和nk-43是蘇聯60年末70年代初由庫茲涅佐夫設計局設計製造的火箭發動機。 用於登月火箭 N1 。 NK-33的 推重比 是當前比沖最高的火箭發動機之一。

A legendary NK-33 (14D15) rocket engine was originally developed to carry Soviet cosmonauts on their way to the Moon onboard a giant N1 rocket. After the ill-fated lunar effort was aborted …

After initial failures of N1 modified engines with multiple ignition capability and increased life were developed. NK-33 was tested at thrust of up to 204 t, variations of components ratio up to 20% …

The NK-33 and NK-43 rocket engines are the highest performing Liquid Oxygen/ Kerosene ever produced. They are upgraded versions of the the NK-15 and NK-15B engines which flew on …

The NK-33 (GRAU index: 14D15) and its vacuum-optimized variant, the NK-43, are rocket engines developed in the late 1960s and early 1970s by the Kuznetsov Design Bureau for the …