The development of the Skif combat laser station, designed to destroy low-orbit space objects with an onboard laser complex, began at NPO Energia, but due to the heavy workload of the association, since 1981, the Skif theme was transferred to the Salyut Design Bureau. August 18, 1983 General Secretary The Central Committee of the CPSU, Yuri Andropov, made a statement that the USSR unilaterally stopped testing the anti-space defense complex. However, with the announcement of the SDI program in the USA, work on the Skif continued.
For testing a laser combat station, a dynamic analogue of the Skif-D was designed. In the future, for the test launch of the Energia launch vehicle, a mock-up sample of the Skif-DM station (Polyus) was urgently created.
The Skif-DM station had a length of 37 meters, a maximum diameter of 4.1 meters and a mass of about 80 tons. It consisted of two main compartments: a smaller one - a functional service unit and a larger one - a target module. The functional unit was a well-developed supply spacecraft for the Salyut orbital station. It housed traffic control systems and on-board complex, telemetry control, command radio communications, thermal regime, power supply, separation and release of fairings, antenna devices, control system for scientific experiments. All devices and systems that could not withstand the vacuum were located in a sealed instrument-cargo compartment. The propulsion unit compartment housed four main engines, 20 orientation and stabilization engines and 16 precision stabilization engines, as well as tanks, pipelines and valves of the pneumohydraulic system serving the engines.
Solar panels were placed on the side surfaces of the propulsion system, which open after entering orbit.
A lot of work has been done in the bureau to create a new large head fairing that protects the functional unit from the oncoming air flow. For the first time it was made of non-metallic material - carbon fiber.
The target module was designed and manufactured from scratch.
At the same time, the designers focused on the maximum use of already mastered nodes and technologies. For example, the diameter and design of all compartments made it possible to use the existing technological equipment of the Khrunichev plant. The nodes connecting the launch vehicle with the spacecraft were taken ready - the same as for the "Buran", as well as the transitional docking block connecting the "Pole" with the Earth at the start. The system for separating the "Polyus" from the rocket also repeated Buranov's.
Since the functional module was essentially a previously mastered spacecraft, it was necessary for it to observe the same loads that it was calculated for when launched by the Proton-K launch vehicle. Therefore, of all the layout options, they were able to choose only one in which the block is located in the head part of the Polus.
And since it was unprofitable to transfer the propulsion system, which was in the functional unit, to the aft part, after separation from the launch vehicle, the Pole flies forward with sustainer engines.
Initially, the launch of the Energia-Skif-DM system was planned for September 1986. However, due to the delay in the manufacture of the apparatus, the preparation of the launcher and other systems of the cosmodrome, the launch was postponed for almost half a year - on May 15, 1987. Only at the end of January 1987, the apparatus was transported from the assembly and test building at the 92nd site of the cosmodrome, where it was trained, to the building of the assembly and refueling complex. There, on February 3, 1987, the Skif-DM was docked with the Energia launch vehicle. The next day, the complex was taken to the universal complex stand-start at the 250th site.
In reality, the Energia-Skif-DM complex was ready for launch only at the end of April.
The flight program of the "Skif-DM" orbital station included ten experiments: four applied and six geophysical ones.
The "VP1" experiment was devoted to the development of a scheme for launching a large-sized spacecraft using a containerless scheme.
In the "VP2" experiment, studies were carried out on the conditions for launching a large-sized apparatus, its structural elements and systems.
Experimental verification of the principles of constructing a large-sized and super-heavy spacecraft (unified module, control systems, thermal control, power supply, electromagnetic compatibility issues) was devoted to the "VPS" experiment.
In the VP11 experiment, it was planned to work out the scheme and technology of the flight.
The program of geophysical experiments "Mirage" was devoted to the study of the effect of combustion products on the upper layers of the atmosphere and ionosphere. The Mirage1 (A1) experiment was to be carried out up to an altitude of 120 kilometers at the launch stage; experiment "Mirage-2" ("A2") - at altitudes from 120 to 280 kilometers during pre-acceleration; experiment "Mirage-3" ("A3") - at altitudes from 280 to the Earth during braking.
Geophysical experiments "GF-1/1", "GF-1/2" and "GF-1/3" were planned to be carried out with the propulsion system of the "Skif-DM" vehicle operating.
The GF-1/1 experiment was devoted to the generation of artificial internal gravity waves in the upper atmosphere.
The purpose of the GF-1/2 experiment was to create an artificial "dynamo effect" in the earth's ionosphere.
Finally, the GF-1/3 experiment was planned to create large-scale ion formations in iono- and plasmaspheres (holes and ducts). To do this, the "Pole" was equipped with a large amount (420 kilograms) of a gas mixture of xenon with krypton (42 cylinders, each with a capacity of 36 liters) and a system for releasing it into the ionosphere.
The launch of the Energia-Skif-DM complex took place on May 15, 1987 with a delay of five hours. Two stages of "Energy" worked successfully. 460 seconds after the launch, the SkifDM separated from the launch vehicle at an altitude of 110 kilometers.
The test program for the Skif-DM apparatus was not fully implemented due to an unfortunate failure that led to the death of the station (I already wrote about this in Chapter 14). However, this flight also gave a lot of results. First of all, all the necessary material was obtained to clarify the loads on the Buran orbital vehicle in order to ensure its flight tests. During the launch and autonomous flight of the vehicle, all four applied experiments (“VP-1”, “VP-2”, “VP-3” and “VP-11”), as well as part of the geophysical experiments (“Mirage-1” and partially "GF-1/1" and "GF-1/3").
The conclusion on the results of the launch stated: “... Thus, the general tasks of launching the product, determined by the launch tasks approved by MOM and UNKS, taking into account the “Decision” of May 13, 1987 to limit the scope of target experiments, were completed by the number of tasks solved by more than 80%".
Combat orbital complex "Skif-DM"
The development of the Skif combat laser station, designed to destroy low-orbit space objects with an onboard laser complex, began at NPO Energia, but due to the heavy workload of the association, since 1981, the Skif theme was transferred to the Salyut Design Bureau. On August 18, 1983, the General Secretary of the Central Committee of the CPSU, Yuri Andropov, made a statement that the USSR would unilaterally stop testing the anti-space defense complex. However, with the announcement of the SDI program in the USA, work on the Skif continued.
For testing a laser combat station, a dynamic analogue of the Skif-D was designed. In the future, for the test launch of the Energia launch vehicle, a mock-up sample of the Skif-DM station (Polyus) was urgently created.
The Skif-DM station had a length of 37 meters, a maximum diameter of 4.1 meters and a mass of about 80 tons. It consisted of two main compartments: a smaller one - a functional service unit and a larger one - a target module. The functional unit was a well-developed supply spacecraft for the Salyut orbital station. It housed the traffic and onboard complex control systems, telemetry control, command radio communications, thermal conditions, power supply, separation and release of fairings, antenna devices, and a control system for scientific experiments. All devices and systems that could not withstand the vacuum were located in a sealed instrument-cargo compartment. The propulsion unit compartment housed four main engines, 20 orientation and stabilization engines and 16 precision stabilization engines, as well as tanks, pipelines and valves of the pneumohydraulic system serving the engines.
Solar panels were placed on the side surfaces of the propulsion system, which open after entering orbit.
A lot of work has been done in the bureau to create a new large head fairing that protects the functional unit from the oncoming air flow. For the first time it was made of non-metallic material - carbon fiber.
The target module was designed and manufactured from scratch.
At the same time, the designers focused on the maximum use of already mastered nodes and technologies. For example, the diameter and design of all compartments made it possible to use the existing technological equipment of the Khrunichev plant. The nodes connecting the launch vehicle with the spacecraft were taken ready - the same as for the "Buran", as well as the transitional docking block connecting the "Pole" with the Earth at the start. The system for separating the "Polyus" from the rocket also repeated Buranov's.
Since the functional module was essentially a previously mastered spacecraft, it was necessary for it to observe the same loads that it was calculated for when launched by the Proton-K launch vehicle. Therefore, of all the layout options, they were able to choose only one in which the block is located in the head part of the Polus.
And since it was unprofitable to transfer the propulsion system, which was in the functional unit, to the aft part, after separation from the launch vehicle, the Pole flies forward with sustainer engines.
Initially, the launch of the Energia-Skif-DM system was planned for September 1986. However, due to the delay in the manufacture of the apparatus, the preparation of the launcher and other systems of the cosmodrome, the launch was postponed for almost half a year - on May 15, 1987. Only at the end of January 1987, the apparatus was transported from the assembly and test building at the 92nd site of the cosmodrome, where it was trained, to the building of the assembly and refueling complex. There, on February 3, 1987, the Skif-DM was docked with the Energia launch vehicle. The next day, the complex was taken to the universal complex stand-start at the 250th site.
In reality, the Energia-Skif-DM complex was ready for launch only at the end of April.
The flight program of the "Skif-DM" orbital station included ten experiments: four applied and six geophysical ones.
The "VP1" experiment was devoted to the development of a scheme for launching a large-sized spacecraft using a containerless scheme.
In the "VP2" experiment, studies were carried out on the conditions for launching a large-sized apparatus, its structural elements and systems.
Experimental verification of the principles of constructing a large-sized and super-heavy spacecraft (unified module, control systems, thermal control, power supply, electromagnetic compatibility issues) was devoted to the "VPS" experiment.
In the VP11 experiment, it was planned to work out the scheme and technology of the flight.
The program of geophysical experiments "Mirage" was devoted to the study of the effect of combustion products on the upper layers of the atmosphere and ionosphere. The Mirage1 (A1) experiment was to be carried out up to an altitude of 120 kilometers at the launch stage; experiment "Mirage-2" ("A2") - at altitudes from 120 to 280 kilometers during pre-acceleration; experiment "Mirage-3" ("A3") - at altitudes from 280 to the Earth during braking.
Geophysical experiments "GF-1/1", "GF-1/2" and "GF-1/3" were planned to be carried out with the propulsion system of the "Skif-DM" vehicle operating.
The GF-1/1 experiment was devoted to the generation of artificial internal gravity waves in the upper atmosphere.
The purpose of the GF-1/2 experiment was to create an artificial "dynamo effect" in the earth's ionosphere.
Finally, the GF-1/3 experiment was planned to create large-scale ion formations in iono- and plasmaspheres (holes and ducts). To do this, the "Pole" was equipped with a large amount (420 kilograms) of a gas mixture of xenon with krypton (42 cylinders, each with a capacity of 36 liters) and a system for releasing it into the ionosphere.
The launch of the Energia-Skif-DM complex took place on May 15, 1987 with a delay of five hours. Two stages of "Energy" worked successfully. 460 seconds after the launch, the SkifDM separated from the launch vehicle at an altitude of 110 kilometers.
The test program for the Skif-DM apparatus was not fully implemented due to an unfortunate failure that led to the death of the station (I already wrote about this in Chapter 14). However, this flight also gave a lot of results. First of all, all the necessary material was obtained to clarify the loads on the Buran orbital vehicle in order to ensure its flight tests. During the launch and autonomous flight of the vehicle, all four applied experiments (“VP-1”, “VP-2”, “VP-3” and “VP-11”), as well as part of the geophysical experiments (“Mirage-1” and partially "GF-1/1" and "GF-1/3").
The conclusion on the results of the launch stated: “... Thus, the general tasks of launching the product, determined by the launch tasks approved by MOM and UNKS, taking into account the “Decision” of May 13, 1987 to limit the scope of target experiments, were completed by the number of tasks solved by more than 80%".
Demetrius Skif
Gay doesn't play hockey.
Part one
Black minstrel.
It happened in a year when an Australian cat named Messiah managed to get a bank card and a loan for more than three thousand US dollars ... It happened in a year when two surgeons in Belgrade got into a fight right during an operation to remove an appendix after one one of them made a remark to another ... It happened in the year when the Kyrgyz parliamentarians, all exclusively men, received flowers as a gift on March 8 from women's organizations ... It happened in the year when the "Dissenting blondes" march was held in Nizhny Novgorod, between twenty and forty people, including brunettes and men ... It happened in a year when a Chinese man married his own photograph, a British man stole a urinal from a pub, and one drunken Polish woman, who was ten months pregnant, managed to give birth to a drunken child ... In general, it happened in the year of the pig ...
The Pink Piranha Club was located in such an inconspicuous gray building that many Muscovites and guests of the capital passed by without paying any attention to it - you never know the offices of obscure and practically unknown firms in Moscow? However, those who were his regular visitors often looked so extravagant that they aroused unhealthy interest in passers-by and law enforcement officers; the latter certainly demanded documents from the visitors of the club. With even greater pleasure, the guardians of the law would have carried out a check of documents inside the "Pink Piranha" in the format of cleaning up the rebellious village, but the authorities (of course, not disinterestedly) did not sanction this action.
Inside the club, everything was kept in pink tones, including the ceiling. Subdued, soft light, passing through pink filters, created an atmosphere in which absolutely foreign bodies the visitors of the Pink Piranha looked like one, all dressed in camouflage of all colors and styles. And only the clothes of waiters and waitresses in the style of BDSM indicated that not a congress of militants was taking place in the club, but fashion party people adhering to, let's say politically correct, non-traditional sexual orientation.
To the left of the bar, in a dim corner of the hall, two people were sitting at a table. The place they took is not very good, between their table and the bar was the entrance to the toilet. Unfortunately, the representatives of the strong (at least from a biological point of view) half of humanity who were sitting here could not find another free place. Here and now, a visitor who was pretty drunk almost collapsed onto the table, and only the speed of reaction of one of the young people saved two already half-empty mugs of beer. An appetizer in the form of pistachios, served instead of a plate in a large ashtray, was not saved by the second. Looking sadly at the broken ashtray and pistachios scattered on the floor, he stood up to his full height, and it must be admitted that he was of considerable height, grabbed the unlucky drunkard by the collar and, giving him acceleration with his foot a little lower than his back, sent him towards the toilet.
Fi, how rude, - remarked his friend, who saved the mugs of beer. - How long have we known each other? And you always try to use brute force at every opportunity.
What do you mean - trying to use brute force? - objected his interlocutor, sitting down in his chair and looking thoughtfully in the direction where he had just sent the poor fellow who violated their privacy, - I just used it.
Remember, a gay doesn't play hockey, - his interlocutor answered this, holding out a mug of beer.
The young man who used this phrase, which later became a catchphrase, was of medium height, thin, black-haired and had a large aquiline nose. His name was Israel Natanovich Zacherman. He was originally from a relatively small town located in the extreme southeast of the European part of Russia.
His father, Natan Moiseevich Zacherman, was a devout Habbadist rabbi who dreamed that his only son would follow in his footsteps in Torah study. To the greatest horror of Natan Moiseevich, his dear Izenka was interested only in dancing, in which he was very successful, and in representatives of his own sex. And if Natan Moiseevich, who lived most of his life under the Soviet Union, could still endure the dances, then he could no longer endure the unconventional inclinations of his dear son. When all calls to come to their senses and begin to be interested not so much in classmates as in classmates, of course, of the corresponding nationality, disappeared in vain, the father closed the gates of his home in front of his son, and at the same time the doors of the only synagogue in the entire district.
Not wanting to quarrel with the only rabbi in the whole district, Izzy's former "friends" and simply "good acquaintances" stopped communicating with him. Very soon, Israel Natanovich Zacherman realized that for a Jew in Russia to be left without the support of the community is the same as becoming Russian. Since, after being expelled from his father's house in his native city of Iza, there was nothing to catch, he, having broken the glass of the synagogue with a stone and painted a swastika on its doors, went to Moscow ...
In Moscow, Mar Israel Natanovich Zacherman joined the Reformed Jewish community, who not only did not condemn sexual attraction to members of their own sex and calmly performed marriage ceremonies between same-sex couples, but even appointed women as rabbis. And now, when religious self-determination was over, the only question arose before the son of the rabbi: what, in fact, to live on? He didn’t have a profession, and he couldn’t have, and he wasn’t going to unload the wagons like some despicable goy. The money was running out fast. Izya was expelled from a rented apartment for debts, and a young representative of the Reformed community decided to trade ... himself.
During his first "appearance" (that is, on the panel), Fira (that was the name of Israel Natanovich in certain circles) met someone who, as subsequent events will show more than once, will play a decisive role in his fate. A strong young man, who answered by the nickname Stepnyak (from the surname Stepnyakov, Russian, non-partisan), at that time had not yet found his vocation in life, although he was a third-year student of the Engineering Chemical Technology Faculty of the Russian Chemical Technology Technical University named after. D.I. Mendeleev. Stepnyak, who at that moment was "slightly" pissed off on the occasion of the surrendered "tail", at first did not even understand what they wanted from him, and then, realizing, he fell into a rage and performed an act of good deed towards Israel. He provided the latter with a free roof over his head along with food, however, in the trauma department of the first city hospital in Moscow. In general, it must be said that Viktor Stepnyakov will become, and not of his own free will, in relation to Israel Natanovich, a kind of executor of the sentences of fate. However, here we are getting ahead of ourselves, but for now Izya meets a male pop diva in the hospital, who "rested" in the next room after a car accident. Common interests and love for music made themselves felt. The rising star of Russian pop music and, concurrently, gay Sasha Sinyan, immediately appreciated all the advantages of Easy. And he, shortly after being discharged, took a worthy place at Sinyan's backup dancer, which he fed from that time ...
Let's return, however, to the Pink Piranha. The excessively pugnacious drinking buddy of Israel Natanovich Zacherman did not share his attitude to hockey. Hockey, as well as much of what was considered "not kosher" among the visitors of the Pink Piranha, he loved. Even more. Stepan Grigoryevich Golushka in childhood, like many boys of primary school age, dreamed of becoming at least a Tretiak. Perhaps Stepan's life would have turned out quite differently if not for his mother, who believed that her dear son simply had to become the next Nureyev.
The development of the Skif laser combat station, designed to destroy low-orbit space objects with an onboard laser complex, began at NPO Energia, but due to the heavy workload of NGOs, since 1981, the Skif theme for creating a laser combat station was transferred to OKB-23 ( KB "Salyut") ( CEO YES. Polukhin). This spacecraft with a laser onboard complex, which was created at the Astrophysics Research and Production Association, had a length of approx. 40 m and weight 95 tons. To launch the Skif spacecraft, it was proposed to use the Energia launch vehicle.
August 18, 1983 General Secretary of the Central Committee of the CPSU Yu.V. Andropov made a statement that the USSR unilaterally stopped testing the PKO complex - after which all tests were stopped. However, with the advent of M.S. Gorbachev and the announcement in the United States of the SDI program, work on anti-space defense continued. For testing a laser combat station, a dynamic analogue of the Skif-D was designed, with a length of approx. 25 m and a diameter of 4 m, in terms of external dimensions, it was an analogue of the future battle station. "Skif-D" was made of thick steel, internal bulkheads supplemented and gained weight. Inside the layout - emptiness. According to the flight program, it was supposed to splash down together with the second stage of Energia in the Pacific Ocean.
In the future, for the test launch of the Energia launch vehicle, a mock-up sample of the Skif-DM station (Pole) was urgently created with a length of 37 m, a diameter of 4.1 m and a mass of 80 tons.
The Polyus spacecraft was conceived in July 1985. precisely as a weight-and-weight model (GVM), with which the first launch of Energia was to be carried out. This idea arose after it became clear that the main load of the rocket - the Buran orbital ship - would not be ready by that date. At first, the task did not seem particularly difficult - after all, making a 100-ton "blank" is not difficult. But suddenly, the Salyut Design Bureau received a wish-order from the Minister of General Mechanical Engineering: to turn the "blank" into a spacecraft for conducting geophysical experiments in near-Earth space and thereby combine the tests of Energia and a 100-ton spacecraft.
In our space industry practice, a new spacecraft has typically been designed, tested, and built for at least five years. But now a completely new approach had to be found. We decided to make the most active use of ready-made compartments, instruments, equipment, already tested mechanisms and assemblies, drawings from other "products".
Machine-building plant them. Khrunichev, who was entrusted with the assembly of the "Polyus", immediately began preparations for production. But these efforts would obviously not be enough if they were not reinforced by the energetic actions of the management - every Thursday the plant held operational meetings held by Minister O.D.Baklanov or his deputy O.N.Shishkin. On these operatives, slow-moving or somewhat dissenting heads of allied enterprises were "rammed" and, if necessary, the necessary assistance was discussed.
No reasons, and even the fact that almost the same team of performers simultaneously carried out a grandiose work on the creation of Buran, as a rule, were not taken into account. Everything was subordinated to keeping deadlines set from above - a vivid example of administrative-command methods of leadership: "strong-willed" idea, "strong-willed" execution of this idea, "strong-willed" deadlines and - "spare no money!"
In July 1986, all compartments, including those newly designed and manufactured, were already at Baikonur.
On May 15, 1987, the super-heavy launch vehicle 11K25 Energia ╧6SL (bench-flying) was launched for the first time from the Baikonur Cosmodrome. The launch became a sensation for the world astronautics. The appearance of a carrier of this class opened up exciting prospects for our country. In its first flight, the Energia carrier rocket carried as a payload an experimental vehicle, the Skif-DM, openly called Polyus.
Initially, the launch of the Energia-Skif-DM system was planned for September 1986. However, due to the delay in the manufacture of the apparatus, the preparation of the launcher and other systems of the cosmodrome, work was delayed by almost half a year - on May 15, 1987. Only at the end of January 1987, the apparatus was transported from the assembly and test building at the 92nd site of the cosmodrome, where it was trained, to the building of the assembly and refueling complex 11P593 at site 112A. There, on February 3, 1987, the Skif-DM was docked with the 11K25 Energia 6SL launch vehicle. The next day, the complex was taken to the universal complex stand-start (UKSS) 17P31 at the 250 site. There began pre-launch joint tests. The completion of the UKSS continued.
In reality, the Energia-Skif-DM complex was ready for launch only at the end of April. All this time, since the beginning of February, the rocket with the device has stood on the launcher. "Skif-DM" was fully fueled, inflated with compressed gases and equipped with on-board power supplies. During these three and a half months, he had to endure the most extreme climatic conditions: temperatures from -27 to +30 degrees, blizzard, sleet, rain, fog and dust storms.
However, the device survived. After extensive preparations, the launch was scheduled for May 12. The first launch of a new system with a promising spacecraft seemed so important to the Soviet leadership that the General Secretary of the Central Committee of the CPSU, Mikhail Sergeevich Gorbachev, was going to honor it with his presence. Moreover, the new leader of the USSR, who took the first post in the state a year ago, had been planning to visit the main cosmodrome for a long time. However, even before Gorbachev's arrival, the leadership of the launch preparations decided not to tempt fate and insure against the "general effect" (any equipment has such a property to break down in the presence of "distinguished" guests). Therefore, at a meeting of the State Commission on May 8, the launch of the Energia-Skif-DM complex was postponed to May 15. It was decided to tell Gorbachev about the technical problems that had arisen. The Secretary General could not wait three more days at the cosmodrome: on May 15, he had already planned a trip to New York to speak at the UN.
On May 11, 1987, Gorbachev flew to the Baikonur Cosmodrome. On May 12, he got acquainted with samples of space technology. The main point of Gorbachev's trip to the cosmodrome was the inspection of Energia with Skif-DM. Then Mikhail Sergeevich spoke to the participants of the upcoming launch.
The Skif-DM flight program included 10 experiments: four applied and 6 geophysical ones. The VP1 experiment was devoted to the development of a scheme for launching a large-sized spacecraft using a containerless scheme. In the VP2 experiment, the conditions for launching a large-sized spacecraft, its structural elements and systems were studied. The VP3 experiment is devoted to the experimental verification of the principles of constructing a large-sized and super-heavy spacecraft (unified module, control systems, thermal control, power supply, electromagnetic compatibility issues). In the VP11 experiment, it was planned to work out the scheme and technology of the flight.
The program of geophysical experiments "Mirage" was devoted to the study of the effect of combustion products on the upper layers of the atmosphere and ionosphere. The Mirage-1 experiment (A1) was to be carried out up to an altitude of 120 km at the launch stage, the Mirage-2 experiment (A2) - at altitudes from 120 to 280 km during re-acceleration, the Mirage-3 experiment (A3) - at altitudes from 280 to 0 km when braking.
Geophysical experiments GF-1/1, GF-1/2 and GF-1/3 were planned to be carried out with the Skif-DM propulsion system operating. The GF-1/1 experiment was devoted to the generation of artificial internal gravity waves in the upper atmosphere. The goal of the GF-1/2 experiment was to create an artificial "dynamo effect" in the earth's ionosphere. Finally, the GF-1/3 experiment was planned to create large-scale ion formations in iono- and plasmaspheres (holes and ducts). "Pole" was equipped with a large amount (420 kg) of a gas mixture of xenon with krypton (42 cylinders, each with a capacity of 36 liters) and a system for releasing it into the ionosphere.
In addition, it was planned to conduct 5 military-applied experiments on the spacecraft, including target shooting, but before the launch, the General Secretary of the CPSU Central Committee M.S. Gorbachev, where he announced the impossibility of transferring the arms race into space, after which it was decided not to conduct military experiments on the Skif-DM spacecraft.
The scheme for launching the Skif-DM apparatus on May 15, 1987 was as follows. 212 seconds after the lift contact at an altitude of 90 km, the head fairing was dropped. This happened as follows: in T + 212 sec, the drives of the fairing longitudinal connector were blown, after 0.3 seconds, the locks of the first group of the GO transverse connector were blown, after another 0.3 seconds, the locks of the second group were blown. Finally, in T + 214.1 sec, the mechanical connections of the head fairing were broken and it was separated.
In T + 460 sec at an altitude of 117 km, the spacecraft and the Energia launch vehicle were separated. At the same time, in T + 456.4 sec, a command was given to switch the four main engines of the launch vehicle to intermediate level traction. The transition took 0.15 seconds. At Т+459.4 sec, the main command was issued to turn off the main engines. Then, after 0.4 sec, this command was duplicated. Finally, at T + 460 sec, a command was issued for the Skif-DM squad. 0.2 sec after that, 16 solid propellant rocket motors were switched on. Then, at T+461.2 sec, the first activation of the solid propellant rocket engine of the SKUS angular velocity compensation system was performed (through the pitch, yaw, and roll channels). The second switching on of the solid propellant rocket engine SKUS, if required, was carried out at T + 463.4 sec (roll channel), the third - at T + 464.0 sec (along the pitch and yaw channels).
51 seconds after separation (T+511 sec), when Skif-DM and Energia were already separated by 120 m, the turn of the apparatus began to issue the first impulse. Since the "Skif-DM" started with the engines forward, it required a 180-degree turn around the transverse Z axis in order to fly with the engines backward. To this turn by 180 degrees, due to the peculiarities of the control system of the device, another “turn” around the longitudinal axis X by 90 degrees was required. Only after such a maneuver, nicknamed by experts as a "reverton", was it possible to accelerate the Skif-DM to enter orbit.
200 seconds were allotted for the "reverton". During this turn, at T+565 sec, a command was given to separate the Skif-DM bottom fairing (separation speed 1.5 m/s). After 3.0 sec (T+568 sec), commands were issued to separate the covers of the side blocks (separation speed 2 m/s) and the covers of the momentless exhaust system (1.3 m/s). At the end of the turn maneuver, the antennas of the onboard radar complex were unchecked, and the covers of the infrared vertical sensors were opened.
At T + 925 sec at an altitude of 155 km, the first activation of four engines for correction and stabilization of the booster compressor station with a thrust of 417 kg was carried out. The operating time of the engines was planned to be 384 sec, the magnitude of the first impulse was 87 m/sec. Then, at T+2220 sec, the deployment of solar panels on the functional service unit "Skif-DM" began. The maximum SB opening time was 60 sec.
The launch of "Skif-DM" was completed at an altitude of 280 km by the second activation of four spacecraft. It was carried out at T + 3605 sec (3145 sec after separation from the launch vehicle). The duration of the engines was 172 seconds, the magnitude of the impulse - 40 m / s. The calculated orbit of the apparatus was planned with a circular height of 280 km and an inclination of 64.6 degrees.
On May 15, the launch was scheduled for 15:00 DMV (16:00 summer Moscow time). On this day already at 00:10 (hereinafter DMV) began and at 01:40 the control of the initial state of the "Skif-DM" was completed. The hydrogen tank of the central block (tank G of block C) of the carrier was preliminarily purged with gaseous nitrogen. At 04:00, the rest of the launch vehicle compartments were purged with nitrogen, and half an hour later, the initial concentration in the hydrogen tank of the C unit was checked. At 07:00, the nitrogen preparation of the fuel tanks of the side blocks was turned on. Refueling of the Energia rocket began at 08:30 (at T-06 hours 30 minutes) from filling the oxidizer tanks (liquid oxygen) of the side and central blocks. The regular cyclogram provided:
- start at the mark T-5 hours 10 minutes refueling the G tank of the central unit with hydrogen (filling time 2 hours 10 minutes);
- at the T-4 hour 40 min mark, start charging the submerged buffer batteries (BB) in the oxygen tanks of the side blocks (block A);
- start charging the submerged BBs in the hydrogen tank of the C block at the T-4 hour 2 min mark;
- at the T-4 hour mark, start refueling the fuel tanks of the side units;
- finish filling the tanks of unit A with liquid oxygen at T-3 hours 05 minutes and turn on their make-up;
- at T-3 hours 02 minutes, complete filling of the central unit with liquid hydrogen;
- at T-3 hours 01 minutes, complete refueling of the side units and turn on the drainage of the filling lines;
- complete refueling of the central unit with oxidizer at T-2 hours 57 minutes.
However, during the refueling of the carrier, technical problems arose, due to which preparations for the launch were delayed by a total of five and a half hours. Moreover, the total delay time was about eight hours. However, the pre-launch schedule had built-in delays, reducing the backlog by two and a half hours.
The delays happened for two reasons. First, a leak was discovered in the detachable joint of pipelines along the line of control pressure for the detachment of the detachable connection for temperature control and firing of the electric board on block 30A due to abnormal installation of the sealing gasket. Correcting this emergency situation took five hours.
Then it was found that one of the two side valves in the liquid hydrogen temperature control line, after issuing an automatic command to close them, did not work. This could be judged by the position of the end contacts of the valve. All attempts to close the valve failed. Both of these valves are fixed to the launch vehicle on the same base. Therefore, it was decided to open a properly closed valve "manually" by issuing a command from the control panel, and then issue a "Closing" command to two valves simultaneously. This would provide mechanical action from a normally operating valve through a common base to the second valve. performing this operation, the “hung” valve received information about its closure.
To be on the safe side, the commands to open and close the valves were repeated manually two more times. Each time the valves closed normally. In the course of further preparations for the launch, the "hung" valve worked normally. However, this emergency situation "pulled out" another hour from the schedule. Another two hours of delays ran up due to malfunctions in some systems of the ground equipment of the universal integrated stand-start.
As a result, only at 17:25 a three-hour readiness for launch was announced, and the input of operational data for the launch began.
At 19:30, hourly readiness was announced. At the T-47 min mark, refueling of the central block of the launch vehicle with liquid oxygen began, which ended after 12 minutes. At 19:55, the set of launch readiness of the apparatus began. Then, in T-21 minutes, the command "Broach 1" passed. After 40 seconds, radio equipment turned on at Energia, and in the T-20 mines, the pre-launch preparation of the carrier began and the adjustment of the kerosene level in the fuel tanks of the side blocks and their pressurization turned on. 15 minutes before the start (20:15), the Skif-DM control system preparation mode was activated.
The "Start" command, which initiates the automatic launch sequence of the launch vehicle, was issued 10 minutes before the launch (20:20). At the same time, the adjustment of the level of liquid hydrogen in the fuel tank of the central unit was turned on, which lasted 3 minutes. 8 minutes 50 seconds before the launch, pressurization and refueling of unit A oxidizer tanks with liquid oxygen began, which also ended after 3 minutes. In T-8 mines, the automation of the propulsion system and pyrotechnics was cocked. In T-3 minutes, the command "Broach 2" was executed. 2 minutes before the launch, a conclusion was received on the readiness of the apparatus for launch. At T-1 min 55 sec, water was to be supplied to cool the gas outlet tray. However, problems arose with this, water did not come in the right amount. 1 min 40 sec before the lifting contact, the engines of the central block were transferred to the "starting position". The pre-pressurization of the side blocks has passed. In T-50 sec, the 2 ZDM service platform was withdrawn. 45 seconds before the launch, the afterburning system of the launch complex was turned on. In T-14.4 sec, the engines of the central block were switched on, in T-3.2 sec, the engines of the side blocks were started.
At 20:30 (21:30 DMV, 17:30 GMT) the "Lift contact" signal passed, platform 3 ZDM departed, and the transitional docking unit separated from Skif-DM. A huge rocket went into the night velvet-black sky of Baikonur. In the first seconds of the flight, a slight panic arose in the control bunker. After separation from the docking-support platform (block I), the carrier made a strong pitching motion in the pitch plane. In principle, this "nod" was predicted in advance by specialists in the control system. It was obtained due to the algorithm incorporated into the Energia control system. After a couple of seconds, the flight stabilized and the rocket went straight up. Subsequently, this algorithm was corrected, and when Energia was launched with Buran, this “nod” was no longer there.
Two stages of "Energy" worked successfully. 460 seconds after the launch, the Skif DM separated from the launch vehicle at an altitude of 110 km. At the same time, the orbit, more precisely, the ballistic trajectory, had the following parameters: the maximum height was 155 km, the minimum height was minus 15 km (that is, the pericenter of the orbit lay under the Earth's surface), the inclination of the trajectory plane to the Earth's equator was 64.61 degrees.
In the process of separation, the system for withdrawing the apparatus with the help of 16 solid propellant rocket motors worked without comment. The disturbances were minimal. Therefore, according to the data of telemetric information, only one solid propellant rocket motor of the angular velocity compensation system along the roll channel was activated, which ensured the compensation of the angular velocity of 0.1 deg/sec along the roll. 52 seconds after the separation, the "reversal" maneuver of the apparatus began. Then, at T+565 sec, the bottom fairing was fired. After 568 seconds, a command was issued to shoot the covers of the side blocks and the protective cover of the SBV. It was then that the irreparable happened: the stabilization and orientation engines of the DSO did not stop the rotation of the apparatus after its regular 180-degree turn. Despite the fact that the "overturn" continued, according to the logic of the program-time device, the separation of the covers of the side blocks and the momentless exhaust system, the opening of the antennas of the "Cube" system, and the shooting of the covers of the infrared vertical sensors took place.
Then, on the rotating Skif-DM, the engines of the DKS turned on. Having failed to reach the required orbital speed, the spacecraft went along a ballistic trajectory and fell in the same place as the central block of the Energia launch vehicle - into the waters of the Pacific Ocean.
Whether the solar panels were opened is not known, but this operation was supposed to take place before the Skif-DM entered the earth's atmosphere. The program-time device of the device worked properly during launch, and therefore, most likely, the batteries opened up. The reasons for the failure were identified at Baikonur almost immediately. In the conclusion on the results of the launch of the Energia Skif-DM complex, it was said:
"... The functioning of all units and systems of the spacecraft ... in the areas of preparation for launch, joint flight with the launch vehicle 11K25 6SL, separation from the launch vehicle and autonomous flight in the first section before launching into orbit passed without remarks. Subsequently, at 568 seconds from the operation of the gearbox (lift contact) due to the passage of an unforeseen cyclogram command of the control system to turn off the power amplifiers of the stabilization and orientation motors (DSO), the product lost its orientation.
Thus, the first boost pulse with a nominal duration of 384 seconds was issued at an outstanding angular velocity (the product made about two complete pitch revolutions) and after 3127 seconds of flight, due to the failure to obtain the required boost speed, it descended into the Pacific Ocean, in the area of the block's impact zone " C" launch vehicle. The depths of the ocean at the site of the fall of the product ... are 2.5-6 km.
The power amplifiers were turned off at the command of the 11M831-22M logic unit upon receipt of a label from the Spektr 2SK on-board time program device (PVU) to reset the covers of the side blocks and protective covers of the momentless exhaust system of the product ... Previously, on products 11F72, this label was used to opening of solar panels with simultaneous blocking of DSO. When redirecting the PVU-2SK tag to issue commands to reset the covers of the BB and SBV of the product ... NPO Elektropribor did not take into account the electrical connection of the 11M831-22M device, blocking the operation of the DSO for the entire area of issuing the first corrective pulse. KB "Salyut" in the analysis of the functional diagrams of the control system developed by NPO "Electropribor" also did not reveal this plot
The reasons for not launching the product ... into orbit are:
a) passage of an unforeseen cyclogram command of the control system to turn off the power amplifiers of the stabilization and orientation engines during a program turn before the first impulse of additional acceleration is issued. Such an emergency situation was not detected during ground testing due to the failure of the lead developer of the control system NPO Elektropribor to check the functioning of the systems and units of the product on a complex stand (Kharkov) ... according to the flight cyclogram in real time.
Carrying out similar work at the manufacturer's CIS, at the Salyut Design Bureau or at the technical complex was impossible because:
- factory complex tests are combined with the preparation of the product at the technical complex;
- a complex stand and an electrical analogue of the product ... were dismantled in the Salyut design bureau, and the equipment was transferred to complete the standard product and the complex stand (Kharkov);
- the technical complex was not equipped with software and mathematical software by the NPO Elektropribor enterprise.
b) The absence in the control system equipment developed by NPO Elektropribor of telemetric information about the presence or absence of power on the power amplifiers of the stabilization and orientation engines.
In the control records, which were made by the recorders during the complex tests, the fact of switching off the power amplifiers of the DSO was accurately recorded. But there was no time left to decipher these records - everyone was in a hurry to launch Energia with Skif-DM.
When the complex was launched, a curious incident occurred. The Yenisei Separate Command and Measurement Complex 4, as planned, began on the second orbit to conduct radio monitoring of the orbit of the launched Skif-DM. The signal on the Kama system was stable. What was the surprise of OKIK-4 specialists when they were told that Skif-DM, without completing even the first orbit, had sunk into the waters of the Pacific Ocean. It turned out that due to an unforeseen error, OKIK received information from a completely different spacecraft. This happens sometimes with the Kama equipment, which has a very wide antenna pattern.
However, the unsuccessful flight of Skif-DM gave a lot of results. First of all, all the necessary material was obtained to clarify the loads on the 11F35OK Buran orbiter to ensure flight tests of the 11F36 complex (the index of the complex consisting of the 11K25 launch vehicle and the 11F35OK Buran orbiter). During the launch and autonomous flight of the vehicle, all four applied experiments (VP-1, VP-2, VP-3 and VP-11), as well as part of the geophysical experiments ("Mirage-1" and partially GF-1/1 and GF -1/3). The Conclusion on the results of the launch stated:
"... Thus, the general launch tasks of the product ..., defined by the launch tasks approved by IOM and UNCS, taking into account the "Decision" of May 13, 1987 on limiting the volume of target experiments, were completed by the number of tasks solved by more than 80%.
The solved tasks cover almost the entire volume of new and problematic solutions, the verification of which was planned at the first start-up of the complex...
The flight tests of the complex as part of the RN 11K25 6SL and the SC "Skif-DM" were for the first time:
- the operability of a super-heavy launch vehicle with an asymmetric lateral location of the launch object was confirmed;
- rich experience gained in ground operation at all stages of preparation for the launch of a super-heavy rocket and space complex;
- obtained on the basis of the telemetric information of the spacecraft ... extensive and reliable experimental data on the launch conditions, which will be used in the creation of spacecraft for various purposes and the ISS "Buran";
- testing of a 100-ton class space platform has begun to solve a wide range of tasks, in the creation of which a number of new progressive layout, design and technological solutions were used.
During the launch of the complex, tests were also carried out on many structural elements, which were later used for other spacecraft and launch vehicles. Thus, the carbon-fiber fairing, first tested in full-scale on May 15, 1987, was later used when launching the Kvant-2, Kristall, Spektr and Priroda modules, and has already been made to launch the first element of the International Space Station - FGB power block.
A May 15 TASS report on this launch stated: "The Soviet Union has begun flight and design tests of a new powerful universal Energia launch vehicle, designed to launch both reusable orbital spacecraft and large-sized spacecraft for scientific and national economic purposes into low-Earth orbits. A two-stage universal launch vehicle... is capable of launching more than 100 tons of payload into orbit... On May 15, 1987, at 21:30 Moscow time, the first launch of this rocket was carried out from the Baikonur Cosmodrome... The second stage of the launch vehicle... The weight-and-weight mock-up of the satellite was brought to the calculated point. After separation from the second stage, the weight-weight mock-up was supposed to be launched into a circular near-Earth orbit using its own engine. However, due to abnormal operation of its onboard systems, the mock-up did not enter the specified orbit and splashed in the Pacific Ocean...
The Skif-DM station, designed to test the design and onboard systems of a combat space complex with a laser, received the index 17F19DM, had a total length of almost 37 m and a diameter of up to 4.1 m, a mass of about 80 tons, an internal volume of approx. 80 cubic meters, and consisted of two main compartments: a smaller one - a functional service unit (FSB) and a larger one - a target module (CM). The FSB was a 20-ton ship, long mastered by the Salyut design bureau and only slightly modified for this new task, almost the same as the transport supply ships Kosmos-929, -1267, -1443, -1668 and the modules of the Mir station ".
It housed the traffic and onboard complex control systems, telemetry control, command radio communications, thermal conditions, power supply, separation and release of fairings, antenna devices, and a control system for scientific experiments. All devices and systems that could not withstand vacuum were located in a sealed instrument-cargo compartment (PGO). In the propulsion unit compartment (ODU) there were four main engines, 20 orientation and stabilization engines and 16 precision stabilization engines, as well as tanks, pipelines and valves of the pneumohydraulic system serving the engines. Solar arrays were placed on the side surfaces of the ODE, opening after entering orbit.
The central unit of the SC "Skif-DM" was adapted with the module of the OKS "Mir-2".
The composition of the remote control module "Skif-DM" included engines 11D458 and 17D58E.
The main characteristics of the launch vehicle "Energia" with the test module "Skif-DM":
Starting weight: 2320-2365 t;
Fuel supply: in side blocks (blocks A) 1220-1240 tons,
in the central block - stage 2 (block C) 690-710t;
Mass of blocks at separation:
lateral 218 - 250 t,
central 78 -86 t;
Weight of the test module "Skif-DM" when separated from the central unit, 75-80 tons;
Maximum velocity head, kg/sq.m. 2500.
Source: site "Space and Rocket Defense Troops",
website " Spaceship"Buran"
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77 t (without modules)
length: 37 m, diameter: 4.1 m
"Pole" (Skif-DM, product 17F19DM) - spacecraft, dynamic layout (DM) of a combat laser orbital platform "Scythian", the payload used during the first launch of the Energia launch vehicle in 1987.
History of creation
Orbital platform "Skif"
"Scythian"- a project for a combat laser orbital platform weighing over 80 tons, the development of which began in the late 1970s at NPO Energia (in 1981, due to the heavy workload of the association, the Skif theme was transferred to the Salyut Design Bureau). On August 18, 1983, the General Secretary of the Central Committee of the CPSU, Yuri Andropov, made a statement that the USSR unilaterally stopped testing the anti-space defense complex, but in connection with the SDI program in the USA, work on the Skif continued.
In particular, a gas-dynamic CO 2 laser GDL RD0600 with a power of 100 kW and dimensions of 2140x1820x680 mm was developed for the laser orbital platform at JSC Design Bureau of Khimavtomatika.
Dynamic layout Skif-DM
In the project's boundaries "Scythian" for 1986-1987, an experimental launch into orbit of a weight-and-weight model of the station (a spacecraft Skif-DM) using a booster "Energy".
Skif-DM had a length of 37 meters, a maximum diameter of 4.1 meters and a mass of about 80 tons. It consisted of two main compartments: a smaller one - a functional service unit and a larger one - a target module. The functional service block was a long-established supply spacecraft for the Salyut orbital station. It housed the traffic and onboard complex control systems, telemetry control, command radio communications, thermal conditions, power supply, separation and release of fairings, antenna devices, and a scientific experiment control system. All devices and systems that could not withstand the vacuum were located in a sealed instrument-cargo compartment.
In the compartment of the propulsion system there were 4 main engines, 20 orientation and stabilization engines and 16 precision stabilization engines, as well as tanks, pipelines and valves of the pneumohydraulic system serving the engines. Solar panels were placed on the side surfaces of the propulsion system, which open after entering orbit.
flight program Skif-DM included ten experiments: four applied and six geophysical.
Launch of the Energia-Skif-DM complex on May 15, 1987
Initially, the launch of the Energia-Skif-DM system was planned for September 1986. However, due to the delay in the manufacture of the apparatus, the preparation of the launcher and other systems of the cosmodrome, the launch was postponed for almost half a year - on May 15, 1987. Only at the end of January 1987, the apparatus was transported from the assembly and test building at the 92nd site of the cosmodrome, where it was trained, to the building of the assembly and refueling complex. There, on February 3, 1987, the Skif-DM was docked with the Energia launch vehicle. The next day, the complex was taken to the universal complex stand-start at the 250th site. In fact, the Energia-Skif-DM complex was ready for launch only at the end of April.
The launch of the complex took place on May 15, 1987 with a delay of five hours. Two stages of "Energy" worked successfully. 460 seconds after the launch, the Skif-DM separated from the launch vehicle at an altitude of 110 kilometers. The process of turning the spacecraft after separation from the launch vehicle due to a switching error electrical circuit lasted longer than expected. As a result, the Skif-DM did not enter the intended orbit and fell into the Pacific Ocean along a ballistic trajectory. Despite this, according to the assessment indicated in the report, more than 80% of the planned experiments were completed.
public message
On May 15, 1987, TASS published a message stating, in part:
| The Soviet Union has begun flight and design tests of a new powerful universal launch vehicle Energia, designed to launch both reusable orbital spacecraft and large-sized spacecraft for scientific and national economic purposes into low-Earth orbits. A two-stage universal launch vehicle ... is capable of launching more than 100 tons of payload into orbit ... On May 15, 1987, at 21:30 Moscow time, the first launch of this rocket was carried out from the Baikonur Cosmodrome ... The second stage of the launch vehicle ... brought the overall weight model to the calculated point satellite. Dimensional-weight layout after separation from the second stage was supposed to be launched into a circular near-Earth orbit with the help of its own engine. However, due to the abnormal operation of its onboard systems, the model did not enter the specified orbit and splashed down in the Pacific Ocean ... |
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Literature
- Glushko V.P. Storming space with rocket systems // . - 3rd ed., revised. and additional - M .: Mashinostroenie, 1987. - S. 304.
Notes
See also
Links
- www.buran.ru/htm/cargo.htm
- www.astronautix.com/craft/polyus.htm
- www.buran.ru/htm/scr.htm - screensaver with a space station and other spacecraft.
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An excerpt characterizing the Pole (spacecraft)
Two hours later the carts were in the courtyard of Bogucharov's house. The peasants were eagerly carrying out and stacking the master's things on the carts, and Dron, at the request of Princess Mary, released from the locker where he was locked up, standing in the yard, disposed of the peasants.“Don’t put it down so badly,” one of the peasants said, A tall man with a round smiling face, accepting the casket from the hands of the maid. She's worth the money too. Why are you throwing it like that or half a rope - and it will rub. I don't like that. And to be honest, according to the law. That's how it is under the matting, but cover it with a curtain, that's important. Love!
“Look for books, books,” said another peasant, who was carrying out the library cabinets of Prince Andrei. - You do not cling! And it’s heavy, guys, the books are healthy!
- Yes, they wrote, they didn’t walk! - a tall chubby man said with a significant wink, pointing to the thick lexicons lying on top.
Rostov, not wanting to impose his acquaintance on the princess, did not go to her, but remained in the village, waiting for her to leave. Having waited for Princess Mary's carriages to leave the house, Rostov mounted on horseback and accompanied her on horseback to the path occupied by our troops, twelve miles from Bogucharov. In Jankovo, at the inn, he took leave of her respectfully, for the first time allowing himself to kiss her hand.
“You’re not ashamed,” blushing, he answered Princess Marya to the expression of gratitude for her salvation (as she called his act), “every guard would have done the same. If we only had to fight with the peasants, we would not let the enemy go so far, ”he said, ashamed of something and trying to change the conversation. “I am only happy to have had the opportunity to meet you. Farewell, princess, I wish you happiness and consolation and wish to meet you under happier conditions. If you don't want to make me blush, please don't thank me.
But the princess, if she did not thank him more with words, thanked him with the whole expression of her face, beaming with gratitude and tenderness. She couldn't believe him, that she had nothing to thank him for. On the contrary, for her it was undoubtedly that if he were not there, then she probably would have to die from both the rebels and the French; that he, in order to save her, exposed himself to the most obvious and terrible dangers; and even more undoubted was the fact that he was a man with a lofty and noble soul, who knew how to understand her position and grief. His kind and honest eyes, with tears coming out of them, while she herself, crying, spoke to him about her loss, did not go out of her imagination.
When she said goodbye to him and was left alone, Princess Mary suddenly felt tears in her eyes, and then, not for the first time, she asked herself a strange question: does she love him?
On the way further to Moscow, despite the fact that the situation of the princess was not joyful, Dunyasha, who was traveling with her in a carriage, noticed more than once that the princess, leaning out of the window of the carriage, smiled joyfully and sadly at something.
“Well, what if I did love him? thought Princess Mary.
No matter how ashamed she was to admit to herself that she was the first to love a man who, perhaps, would never love her, she consoled herself with the thought that no one would ever know this and that it would not be her fault if for the rest of her life, no one talking about loving the one she loved for the first and last time.
Sometimes she remembered his views, his participation, his words, and it seemed to her that happiness was not impossible. And then Dunyasha noticed that she, smiling, was looking out the window of the carriage.
“And he should have come to Bogucharovo, and at that very moment! thought Princess Mary. - And it was necessary for his sister to refuse Prince Andrei! - And in all this, Princess Mary saw the will of providence.
The impression made on Rostov by Princess Marya was very pleasant. When he thought about her, he felt merry, and when his comrades, having learned about the adventure that had happened with him in Bogucharov, joked to him that he, having gone for hay, had picked up one of the richest brides in Russia, Rostov became angry. He was angry precisely because the idea of marrying a pleasant for him, meek Princess Marya with a huge fortune more than once came to his mind against his will. For himself, Nikolai could not wish for a better wife than Princess Mary: marrying her would make the Countess, his mother, happy, and improve his father’s affairs; and even—Nikolai felt it—would have made Princess Marya happy. But Sonya? AND given word? And this made Rostov angry when they joked about Princess Bolkonskaya.
Having taken command of the armies, Kutuzov remembered Prince Andrei and sent him an order to arrive at the main apartment.
Prince Andrei arrived in Tsarevo Zaimishche on the very day and at the very time of the day when Kutuzov was making the first review of the troops. Prince Andrei stopped in the village near the priest's house, where the commander-in-chief's carriage was stationed, and sat down on a bench at the gate, waiting for the Serene Highness, as everyone now called Kutuzov. On the field outside the village, one could hear the sounds of regimental music, then the roar of a huge number of voices shouting “Hurrah! to the new commander-in-chief. Immediately at the gate, about ten paces from Prince Andrei, taking advantage of the absence of the prince and the fine weather, stood two batmen, a courier and a butler. Blackish, overgrown with mustaches and sideburns, a little hussar lieutenant colonel rode up to the gate and, looking at Prince Andrei, asked: is the brightest here and will he be soon?
Prince Andrei said that he did not belong to the headquarters of his Serene Highness and was also a visitor. The hussar lieutenant colonel turned to the well-dressed batman, and the batman of the commander-in-chief said to him with that special contempt with which the batmen of the commanders-in-chief speak to the officers:
- What, brightest? It must be now. You that?
The hussar lieutenant colonel grinned into his mustache at the orderly, got off the horse, gave it to the messenger and went up to Bolkonsky, bowing slightly to him. Bolkonsky stood aside on the bench. The hussar lieutenant-colonel sat down beside him.
Are you also waiting for the commander-in-chief? said the hussar lieutenant colonel. - Govog "yat, accessible to everyone, thank God. Otherwise, trouble with the sausages! Nedag" om Yeg "molov in the Germans pg" settled down. Tepeg "maybe and g" Russian talk "it will be possible. Otherwise, Cheg" does not know what they were doing. Everyone retreated, everyone retreated. Did you do the hike? - he asked.
- I had the pleasure, - answered Prince Andrei, - not only to participate in the retreat, but also to lose in this retreat everything that he had dear, not to mention the estates and home... a father who died of grief. I am from Smolensk.
- And? .. Are you Prince Bolkonsky? It’s very cool to meet you: Lieutenant Colonel Denisov, better known by the name of Vaska, Denisov said, shaking Prince Andrei’s hand and peering into Bolkonsky’s face with especially kind attention. Yes, I heard, ”he said sympathetically and, after a pause, continued : - Here is the Scythian war. This is all hog "osho, but not for those who puff with their sides. And you are Prince Andg "she Bolkonsky?" He shook his head. "Very hell, prince, very hell to meet you," he added again with a sad smile, shaking his hand.
Prince Andrei knew Denisov from Natasha's stories about her first fiancé. This recollection both sweetly and painfully carried him now to those painful sensations of which he Lately I had not thought about it for a long time, but which were still in his soul. Recently, there have been so many other and such serious impressions as leaving Smolensk, his arrival in the Bald Mountains, recently known about the death of his father - so many sensations were experienced by him that these memories had not come to him for a long time and, when they did, had no effect on him. him with the same strength. And for Denisov, the series of memories that Bolkonsky’s name evoked was the distant, poetic past, when, after dinner and Natasha’s singing, without knowing how, he proposed to a fifteen-year-old girl. He smiled at the memories of that time and his love for Natasha, and immediately turned to what passionately and exclusively now occupied him. This was the campaign plan he had come up with while serving in the outposts during the retreat. He presented this plan to Barclay de Tolly and now intended to present it to Kutuzov. The plan was based on the fact that the French line of operations was too long and that instead of, or at the same time, acting from the front, blocking the way for the French, it was necessary to act on their messages. He began to explain his plan to Prince Andrei.
