The RD-0124 (Russian: Ракетный Двигатель-0124, romanized: Raketnyy Dvigatel-0124, lit. 'Rocket Engine 0124', GRAU index: 14D23) is a rocket engine burning liquid oxygen and kerosene in an oxygen-rich staged combustion cycle, developed by the Chemical Automatics Design Bureau in Voronezh.

RD-0124 engine. The 30-ton-thrust RD-0124 engine developed for the Soyuz-2 launcher would have roughly same dimensions (height: 2,327 millimeters, diameter: 1,470 millimeters) and the basic design as the veteran RD-0110 engine on the third stage of the previous Soyuz rockets. The main difference would be the introduction of the so-called closed ...

rd-0124是俄罗斯在rd-0110基础上研制的液氧煤油发动机。 其相比RD-0110，取消了游机，更改了推力矢量控制方式和循环方式，性能更高，用于联盟2.1B、联盟2.1V和 安加拉 系列的URM-2二级。

There was also the RD-0124, which is a closed cycle engine that the Soviets intended to use universally on several vehicles. It did not have any vernier engines and used RG-1 instead of the usual T-1 kerosene.

Kosberg LOx/Kerosene rocket engine. In development. Engine to succeed RD-0110 in second stage of Soyuz. Used staged combustion; chamber pressure increased from 70 to 160 bar, specific impulse from 326 to 359 seconds. First flight 2001. Proposed for small launcher Kvant-1 by RKK Energia for stage 1 steering engine.

2021年11月24日 · RD-0124. There was also the RD-0124, which is a closed cycle engine that the Soviets intended to use universally on several vehicles. It did not have any vernier engines and used RG-1 instead of the usual T-1 kerosene. This closed cycle engine offered an improved ISP of 359 s instead of 326 s, which was practical for larger payloads.

2020年2月12日 · 在沃罗涅日市中心 火箭 NPO Energomash 旗下的发动机制造公司开始对最新的俄罗斯火箭发动机 RD0124MS 进行点火测试。 Energomash 新闻部门报道了这一消息。 根据该报告，在该企业的消防局对第一座喷嘴缩短的发电厂进行了两次成功的燃烧试验。 试验证实了燃烧室在减压下的稳定性。 第二座发电厂也正在准备进行测试。 在测试完两个安装之后，专家将继续测试发动机组件。 如新闻服务中所述，新的RD0124MS火箭发动机是在RD0124A发动机的基础 …

Three variations of the Soyuz-5 rocket as of 2013 and 2014. Each module of the first stage would be equipped with a single RD-0164 engine burning liquid methane. An upper stage would feature RD-0124 engine modified for methane fuel and developing a thrust of 30 tons.

Двигатель РД-0124 выполнен по схеме с дожиганием окислительного генераторного газа и включает в себя четыре камеры сгорания, газогенератор, систему подачи компонентов топлива (ТНА и бустерные насосные агрегаты горючего и окислителя), систему запуска и выключения, систему регулирования и управления, …

2006年12月27日 · RD-0124 （ GRAU指数14D23）是由Voronezh的化学自动化设计局开发的富含氧气的燃烧周期的火箭发动机燃烧液体氧和煤油。 RD-0124发动机用于SOYUZ-2.1B和SOYUZ-2-1V 。