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一、任务的简要特点,内容和研究结果 由于在真空条件下起动时的压力峰引起了。呵波罗》飞船眼务舱的空间姿态控制系统发动机（推力为45.4公斤）的破坏（此时喷管是位于向上状态）。因此,发动机的研制公司和载人宁宙飞行器中心进行了广泛的研究来寻找失败的原因,以便采取必要的措施来防止未来出现这样的情况。 由于在飞行器加速运动时和在月球附近进行机动时,发动机是处在过载作用状态,因此需要究研发动机相对过载作用方向的定向时对其起动特性的影响。 载人宇宙飞行器中心的究研计划分为两个阶段,并于1966年6-9月完成。第一阶段包括各种试验性的研究,其目的是确定发动机在真空起动时（其喷管向上放置）压力急剧上升形成的过程及其机理,并对各个量对此现象的影响进行初步判断。第二阶段是对各参量影
First, the task of the brief characteristics, content and research results due to pressure conditions at the start of the vacuum caused by the peak. Babylon "spacecraft eye space attitude control system engine (thrust 45.4 kg) damage (at this time the nozzle is located in the up state). Therefore, the engine development company and the manned spacecraft center conducted extensive research to find out the reasons for the failure so that the necessary measures could be taken to prevent such a situation in the future. Since the engine is in an overloaded state during maneuvering of the aircraft and during maneuvering around the moon, it is necessary to study the influence of the orientation of the relative overloading action on the starting characteristics of the aircraft. The research program of the manned spacecraft center was divided into two phases and was completed in June-September 1966. The first phase includes a variety of experimental studies aimed at determining the process and mechanism by which the pressure of the engine rises sharply at the start of the vacuum (the nozzle is placed upwards), and to make a preliminary assessment of the effect of each quantity on this phenomenon. The second stage is the shadow of the parameters