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Kirillov, Anatoli Semenovich
Russian officer. Chief of the First Directorate of Baikonur 1960-1967.

Born: 1924-12-31. Died: 1987-03-30.

After World War II service, served in Far East. Dzerzhinsky Academy 1949-1955. Thereafter assigned to Baikonur, where he oversaw launch teams. Deputy Commander at Baikonur for space matters, 1967-1969. Deputy Commander of GUKOS for political matters from 1970, completing career in a senior staff position in the VKS from 1976.

Country: Russia. Spacecraft: Vostok, Voskhod. Projects: Lunar L3. Agency: RVSN. Bibliography: 474.

1924 December 31 - .
  • Birth of Anatoli Semenovich Kirillov - . Nation: Russia. Related Persons: Kirillov. Russian officer. Chief of the First Directorate of Baikonur 1960-1967..

1961 March 25 - . 05:54 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Vostok 8K72K.
  • Korabl-Sputnik 5 - . Payload: Vostok 3KA s/n 2. Mass: 4,695 kg (10,350 lb). Nation: Russia. Related Persons: Bykovsky, Gagarin, Goreglyad, Kamanin, Karpov, Keldysh, Kirillov, Korolev, Nelyubov, Nikolayev, Popovich, Titov, Voskresenskiy, Yazdovskiy. Agency: RVSN. Program: Vostok. Class: Manned. Type: Manned spacecraft. Flight: Vostok 1. Spacecraft Bus: Vostok. Spacecraft: Vostok. Duration: 0.0600 days. Decay Date: 1961-03-25 . USAF Sat Cat: 95 . COSPAR: 1961-Iota-1. Apogee: 175 km (108 mi). Perigee: 175 km (108 mi). Inclination: 64.9000 deg. Period: 88.00 min.

    Carried dog Zvezdochka and mannequin Ivan Ivanovich. Ivanovich was again ejected from the capsule and recovered by parachute, and Zvezdochka was successfully recovered with the capsule on March 25, 1961 7:40 GMT.
    Officially: Development of the design of the space ship satellite and of the systems on board, designed to ensure man's life functions during flight in outer space and return to Earth. Additional Details: here....

1962 August 11 - . 08:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Vostok 8K72K.
  • Vostok 3 - . Call Sign: Sokol (Falcon ). Crew: Nikolayev. Backup Crew: Bykovsky, Volynov. Payload: Vostok 3KA s/n 5. Mass: 4,722 kg (10,410 lb). Nation: Russia. Related Persons: Barmin, Bykovsky, Gagarin, Khrushchev, Kirillov, Kozlov, Frol, Nikolayev, Popovich, Smirnov, Ustinov, Volynov. Agency: RVSN. Program: Vostok. Class: Manned. Type: Manned spacecraft. Flight: Vostok 3. Spacecraft Bus: Vostok. Spacecraft: Vostok. Duration: 3.93 days. Decay Date: 1962-08-15 . USAF Sat Cat: 363 . COSPAR: 1962-A-Mu-1. Apogee: 218 km (135 mi). Perigee: 166 km (103 mi). Inclination: 65.0000 deg. Period: 88.30 min.

    Joint flight with Vostok 4. The first such flight, where Vostok capsules were launched one day apart, coming within a few kilometers of each other at the orbital insertion of the second spacecraft. The flight was supposed to occur in March, but following various delays, one of the two Vostok pads was damaged in the explosion of the booster of the third Zenit-2 reconnsat in May. Repairs were not completed until August. Vostok 3 studied man's ability to function under conditions of weightlessness; conducted scientific observations; furthered improvement of space ship systems, communications, guidance and landing. Immediately at orbital insertion of Vostok 4, the spacecraft were less than 5 km apart. Popovich made radio contact with Cosmonaut Nikolayev. Nikolayev reported shortly thereafter that he had sighted Vostok 4. Since the Vostok had no maneuvering capability, they could not rendezvous or dock, and quickly drifted apart. The launches did allow Korolev to offer something new and different, and gave the launch and ground control crews practice in launching and handling more than one manned spacecraft at a time. The cosmonaut took colour motion pictures of the earth and the cabin interior. Additional Details: here....

1963 June 14 - .
  • Vostok 5 Launch - . Nation: Russia. Related Persons: Bykovsky, Gagarin, Khrushchev, Kirillov, Korolev, Pilyugin, Tyulin. Flight: Vostok 5. Spacecraft Bus: Vostok. Spacecraft: Vostok.

    At 8 am the State Commission meets and approves a five-hour countdown to launch of Vostok 5 at 14:00. The cosmonaut and his backup have slept well and are at medical at 9:00 for the pre-flight physical examination and donning of their space suits. At T minus 2 hours and fifteen minutes they ride the bus to the pad. A few minutes after Bykovskiy is inserted into the capsule, problems with the UHF communications channels are encountered - three of the six channels seem to be inoperable. Gagarin and Odintsov are consulted on how it will be for the cosmonaut to fly with just three channels operable - is it a Go or No-Go? Go! Next a problem develops with the ejection seat. After the hatch is sealed, a technician cannot find one of the covers that should have been removed from the ejection seat mechanism. It is necessary to unbolt the hatch and check - the seat will not eject if the cover has been left in place. At T minus 15 minutes Gagarin, Korolev, Kirillov, and Kamanin go into the bunker adjacent to the rocket.

    A new problem arises -- the 'Go' light for the Block-E third stage won't illuminate on the control room console. It can't be determined if it is a failure of the stage or an instrumentation failure. It will take two to five hours to bring up the service tower and check out the stage. But if the rocket is left fuelled that long, regulations say it must be removed from the pad and sent back to the factory for refurbishment. In that case there can be no launch until August. Krylov and the State Commission would rather defer the launch to August. The last possible launch time is 17:00 in order to have correct lighting conditions for retrofire and at emergency landing zones. But Korolev, Tyulin, Kirillov, and Pilyugin have faith in their rocket, decide that the problem must be instrumentation, and recycle the count for a 17:00 launch.

    The launch goes ahead perfectly at 17:00 - even all six UHF communications channels function perfectly. On orbit 4 Bykovskiy talks to Khrushchev from orbit and good television images are received from the capsule. Bykovskiy reports he can see the stars but not the solar corona. His orbit is good for eleven days.

1964 October 6 - . 07:12 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 47 - . Payload: Voskhod 3KV s/n 2. Mass: 5,320 kg (11,720 lb). Nation: Russia. Related Persons: Kirillov, Korolev, Rudenko, Tyulin. Agency: Korolev Design Bureau. Program: Voskhod. Class: Manned. Type: Manned spacecraft. Flight: Voskhod 1. Spacecraft Bus: Vostok. Spacecraft: Voskhod. Duration: 1.01 days. Decay Date: 1964-10-07 . USAF Sat Cat: 891 . COSPAR: 1964-062A. Apogee: 383 km (237 mi). Perigee: 174 km (108 mi). Inclination: 64.6000 deg. Period: 90.10 min.

    Unmanned test of Voskhod spacecraft. At 07:00 the State Commission meets at Area 2. All Chief Designers, Commanders, and Section report that all is ready for flight. The commission gives the order to proceed with the launch. Weather at the pad is 7 balls, 8-10 m/s wind with gusts to 15 m/s, temperature 9 to 12 deg C. Weather in the recovery zones is reported as winds up to 15 m/s. Weather in the recovery zone is not clear, but that is not considered an impediment, and in fact Kamanin would like to see how the landing system functions in bad conditions. Kamanin visits the pad at T-30 seconds; at T-20 seconds, the veranda at IP-1 has over 50 viewers of the launch, including 15 cosmonaut candidates and the 7 Voskhod cosmonauts. Kamanin is relegated to the IP-1 veranda this time, with Rudenko, Kirillov, and Tyulin the bunker adjacent to the pad. Korolev stays with the booster until T-5 minutes, then enters the bunker. The booster ignites precisely at 10:00; the strap-ons burn out and are jettisoned at T+120 seconds; the core burns out and the final stage ignites at T+290 seconds; and at T+523 seconds spacecraft 3KV number 2 is placed in orbit as the final stage shuts down. The spacecraft separates and all systems look normal.

    Recovered October 7, 1964 7:28 GMT. Officially: Investigation of the upper atmosphere and outer space.

1964 October 13 - .
1966 November 17 - .
  • VVS told to surrender on crew assignments issue. - . Nation: Russia. Related Persons: Bykovsky, Kerimov, Khrunov, Kirillov, Komarov, Kuznetsov, Mishin, Rudenko, Yeliseyev, Zakharov. Program: Soyuz, Lunar L1. Flight: Soyuz 1, Soyuz 2A, Soyuz 7K-L1 mission 1.

    Kamanin is at Tyuratam for the first Soyuz launch. He and Rudenko are accommodated in the new hotel at Area 2. It has all conveniences - a local telephone, radio and television with Moscow programs, even a promise to install an HF telephone that will allow secure communications with Moscow. Also there for the launch are Kerimov, Kirillov, Kuznetsov, Bykovsky, Komarov, Khrunov, amd Yeliseyev. Rudenko reports that he has been chewed out by Marshal Zakharov. Zakharov told him "What are you and Kamanin doing, blocking OKB-1 candidates from flight? If Mishin wants to send his people to the Moon, let him do it and do not interefere!"

1966 December 15 - .
  • Soyuz failure in detail - . Nation: Russia. Related Persons: Kerimov, Kirillov, Mishin. Program: Soyuz. Flight: Soyuz 1, Soyuz 2A. Spacecraft Bus: Soyuz. Spacecraft: Soyuz 7K-OK.

    Kerimov, Mishin, and Kirillov were nearly scared to death but escaped unharmed. A fuller account of yesterday's events is available. At the command "ignition", only the second stage engines of the core vehicle ignited; the first stage strap-ons did not, therefore the rocket did not develop enough thrust to move an inch. On the order to flood the pad, all power was cut off to the rocket and equipment. 35-40 minutes after shutdown of the booster and the flooding, only steam and oxygen vapour were rising from the pad. Mishin and Kirillov emerged from the bunker and approached the rocket. They decided the danger was past, and gave the command for the service gantries to be raised, to protect the rocket from wind gusts. As the gantry arms reached the upper stage, and personnel were climbing up to service the rocket, one arm tilted the dislocated rocket more than seven degrees from the vertical. At such an angle the SAS abort sequence was activated. The solid rockets of the SAS abort motor suddenly ignited, pulling the Soyuz capsule 600 m into the sky, but also setting the third stage of the rocket on fire. This immediately alerted Mishin, Kerimov, and Kirillov to take cover in the bunker, while others were able to run to 100 to 200 m from the pad in the two minutes before the first stage exploded. A Major Korostylev and a group of soldiers decided instead to take cover behind the concrete wall of the pad, and paid for this decision with their lives or severe injuries. A preliminary accident commission meeting was convened at 09:00 at Area 2. An oxygen bypass valve failure several seconds after the ignition command is blamed for the shutdown of the first-stage engines. Although final acceptance tests of the SAS tower only began at Vladimirovka on 10 December, it is noted that the SAS system has actually just passed its most realistic test - it saved the Soyuz capsule, which landed 300 meters from the pad. Examining the blackened and smoking pad later, it is estimated it will take at least six months to get it back into operation.

1968 October 22 - .
  • Soyuz 2/3 State Commission. - . Nation: Russia. Related Persons: Barmin, Glushko, Keldysh, Kirillov. Program: Soyuz. Flight: Soyuz 3. Soyuz 2/3 State Commission. All the 'grey eminences' are there - Keldysh, Barmin, Glushko, Kirillov, etc. There are a huge number of physicians - 22 from the VVS, 100 from Minzdrav - all to check the single cosmonaut..

1969 February 21 - . 09:18 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC110R. LV Family: N1. Launch Vehicle: N-1 11A52. FAILURE: First stage failure.. Failed Stage: 1.
  • N1 3L launch - . Payload: Soyuz 7K-L1S s/n 3. Mass: 6,900 kg (15,200 lb). Nation: Russia. Related Persons: Afanasyev, Sergei, Dorofeyev, Kirillov, Mishin. Agency: RVSN. Program: Lunar L3. Class: Manned. Type: Manned spacecraft. Spacecraft Bus: Soyuz. Spacecraft: Soyuz 7K-L1A. Decay Date: 1969-02-21 . Apogee: 30 km (18 mi).

    N-1 serial number 3L was the first N-1 launched. The vehicle ran into trouble immediately at lift-off. A fire developed in the tail compartment. The engine monitoring system detected the fire, but then gave an incorrect signal, shutting down all engines at 68.7 seconds into the flight. British intelligence detected the launch attempt, but the CIA's technical means for some reason missed it and they denied for years that it had ever occurred. In retrospect the launch team at Baikonur pointed to a grave mistake - at the christening of the first N1, the champagne bottle broke against the crawler-transporter rather than the hull of the rocket. After the 3L failure everyone knew there was no chance at all of beating the Americans to the moon. Additional Details: here....

1987 March 30 - .
  • Death of Anatoli Semenovich Kirillov - . Nation: Russia. Related Persons: Kirillov. Russian officer. Chief of the First Directorate of Baikonur 1960-1967..

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