Мы закончили первую стадию испытани

Мы закончили первую стадию испытаний нашего ускорителя первой ступени "Большая мамочка".
К сожалению, в ходе испытаний мы потеряли один из двух ускорителей из-за ошибки автоматического управления посадкой ступени в стартовую точку. На данный момент ошибка исправлена и тесты второго прототипа ступени это подтверждают.
Итог испытания ускорителя в штате Техас такой: запуск прототипа один и прототипа два на 200 метров с приземлением - миссия прошла успешно. Запуск прототипа один на 500 метров - миссия провалена, взрыв ускорителя из-за слишком высокой скорости приземления. Запуск прототипа 2 на 500 метров после коррекции - миссия прошла успешно. Наконец, запуск ускорителя на 1000 метров и последующий спуск к точке запуска - миссия прошла успешно.
Целью данного ускорителя, названного "Большая мамочка" в том, чтобы на начальном этапе за очень ограниченное время придать максимальное ускорение основной ракете.
Это позволит включить более экономные двигатели второй ступени, имея хороший запас скорости. Что в итоговом результате выльется в хорошую экономию топлива и возможность использования на второй ступени более надежных двигателей.
Однако, такое исполнение также содержит несколько минусов. Во-первых, сложность такой конструкции и потенциально большое количество проблемных участков на первой ступени. Во-вторых, чрезмерное ускорение, которое за время работы ступени может достигать 20 G. Наконец, такой подход к ракетостроению еще не использовался и нас, как первопроходцев, может ожидать много неудач.

Результаты (английский) 1:

We finished the first stage of testing of our first stage Accelerator "big mom". Unfortunately, during the tests we have lost one of the two accelerators due to error of automatic control landing stage at the starting point. At the moment, the bug has been fixed and the second-stage prototype tests confirm it.Total test accelerator in Texas: one prototype and prototype to run two at 200 yards with a touchdown-the mission was successful. The launch of the prototype one on 500 meters-mission failed, the explosion of the accelerator because of too high speed landing. Launch of prototype 2 on 500 meters after the correction-the mission was successful. Finally, launch Accelerator at 1000 meters and the subsequent descent to the start point of the mission was successful.The purpose of this accelerator, called "Big mother" to initially for a very limited time give maximum acceleration a primary projectile. This will include more fuel-efficient engines, having a good supply of speed. That outcome will result in good fuel economy and ability to use on the second stage more reliable engines. However, this design also contains a few downsides. Firstly, the complexity of this design and a large number of potentially problematic areas in the first stage. Secondly, excessive speeding, which during the work steps can reach 20 G. Finally, this approach to missile monitoring teams have not made and us as pioneers, can expect many failures.

Результаты (английский) 2:

We have completed the first stage of our test of the first stage of the accelerator "Big Mama".
Unfortunately, in the course of testing, we have lost one of the two accelerators due to an error of automatic control landing stage to the starting point. At this point the error is corrected, and the tests of the second prototype stage is confirmed.
The result of the accelerator tests in the state of Texas is this: launch of the prototype and a prototype two on the 200 meters with a touchdown - the mission was successful. Running a prototype at 500 meters - mission failed, the accelerator explosion because of too high landing speed. Launch of the prototype 2 500 meters after the correction - the mission was successful. Finally, the launch of the accelerator at 1000 meters and the subsequent descent to the point of run - the mission was successful.
The aim of the accelerator called the "Big Mama" to the initial stage for a very limited time to give maximum acceleration of the main rocket.
This will enable more fuel-efficient engines the second stage, with a good supply of speed. What is the final result will result in good fuel economy and the use of the second stage more reliable engines.
However, such performance also has a few drawbacks. Firstly, the complexity of this design and the potentially large number of problem areas in the first stage. Secondly, excessive acceleration, which during the operation stage may reach 20 G. Finally, this approach to the rocket production has not yet been used, and us as pioneers can expect a lot of failures.

Результаты (английский) 3:

we finished the first stage of testing our booster first stage "big mama".unfortunately, in the course of testing, we have lost one of the two accelerators because of errors in the starting point of automatic control landing stage. at this time, the bug has been fixed and the second prototype level tests confirmed it.the test sequence in the state of texas. the prototype and prototype of two 200 meters from the landing - the mission was a success. the prototype of a 500 meters - the mission was a failure, the accelerators because of too high speed landing. the prototype of 2 500 meters after the correction, the mission was a success. finally, the accelerator at 1000 meters, and subsequent to the launch of the mission was a success.the purpose of this accelerator, called "big mama" is to initially for a very limited time to the maximum acceleration of the rocket.this will include a more efficient engines, the second level having a good supply of speed. the outcome will be a good fuel efficiency and the possibility to use in the second stage a more reliable engines.however, this design also contains a few weaknesses. first, the complexity of the structure and potentially a large number of critical sections in the first level. secondly, the excessive acceleration, which during the working cycle can be as high as 20 g. finally, an approach to ракетостроению still used as pioneers, and we can expect many failures.