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The Circolo Canottieri Aniene, aware of the role that sport plays in the growth and development of young people, is increasingly aimed at disseminating precisely this, training young people to be the athletes of tomorrow, but above all transmitting our passion for the sport.

Subtopics RT-15M Russian submarine-launched ballistic missile. Under the original resolution in 1961 starting the RT-2 program, Makeyev was to develop a submarine-launched version of the RT-15, consisting of the first and second stages of the RT-2. It did not proceed beyond the study stage. Family: IRBM, vehicle-launched. Country: Russia. Launch Sites: Kapustin Yar, Kapustin Yar LC84, Kapustin Yar V-2. Stages: 15D94, 15D27. Agency: Arsenal. Bibliography: 2, 475, 476, 8553. Photo Gallery RT-15 1965 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1965 September 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC84. Launch Pad: LC84?. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). November 1966 - . Launch Site: Kapustin Yar. LV Family: RT-2. Launch Vehicle: RT-15. First RT-15 launch in regiment test series. - . Nation: Russia. Agency: RVSN. 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1970 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1970 March 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

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In 1892, the Circolo Canottieri Aniene was founded by Alessandro Morani and the Fasoli brothers. The historic crew of the first ‘yole’ (a four-place rowboat), known as ‘Rugantino’, collected their first prestigious laurels, rapidly raising the profile of the Circolo Canottieri Aniene in Rome and throughout Italy.

The Circolo Canottieri Aniene has now become a social and sporting reality of absolute value in both the Italian and international arena thanks to the passionate activity of its members, management, technicians and athletes.

U.S. Route15

Precisely in virtue of and as an acknowledgement to this constant commitment, on 23 January 2002, the Prime Minister, at CONI’s proposal, awarded the Circolo Canottieri Aniene with the Collare d’Oro, our country’s highest honour in the sports field, becoming the first and only sports club to obtain this recognition.

Maximum range: 2,500 km (1,500 mi). Number Standard Warheads: 1. Warhead yield: 50 KT. CEP: 2.26 km (1.40 mi). Boost Propulsion: Solid rocket. Initial Operational Capability: 1970. Total Number Built: 19. Subtopics RT-15M Russian submarine-launched ballistic missile. Under the original resolution in 1961 starting the RT-2 program, Makeyev was to develop a submarine-launched version of the RT-15, consisting of the first and second stages of the RT-2. It did not proceed beyond the study stage. Family: IRBM, vehicle-launched. Country: Russia. Launch Sites: Kapustin Yar, Kapustin Yar LC84, Kapustin Yar V-2. Stages: 15D94, 15D27. Agency: Arsenal. Bibliography: 2, 475, 476, 8553. Photo Gallery RT-15 1965 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1965 September 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC84. Launch Pad: LC84?. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). November 1966 - . Launch Site: Kapustin Yar. LV Family: RT-2. Launch Vehicle: RT-15. First RT-15 launch in regiment test series. - . Nation: Russia. Agency: RVSN. 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1970 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1970 March 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

Confirming that it always remains faithful to the motto ‘sportsmanship, cordiality and spirit of tradition’ that inspired its founders in 1892, the Circolo Canottieri Aniene today, like then, seizes every opportunity that embodies the harmony between sports and solidarity, actively engaging its compassionate and ever-present members in these remarkable events, destined to enter into the memories of those who proudly represent its social body.

The history and tradition of our Club stand as a remarkable testimony to the inseparable and captivating bond existing between the city of Rome and its river.

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AKA: 15P696;8K96;Scamp;Scapegoat (Scamp);SS-14. Status: Retired 1970. First Launch: 1965-01-01. Last Launch: 1970-03-01. Number: 19 . Payload: 500 kg (1,100 lb). Thrust: 412.00 kN (92,621 lbf). Gross mass: 16,000 kg (35,000 lb). Height: 11.90 m (39.00 ft). Diameter: 1.49 m (4.88 ft). Apogee: 500 km (310 mi). Decree 316-157 of 4 April 1961 authorized development of a family of solid propellant launch vehicles utilizing various combinations of three stages (the RT-2, RT-15, and RT-25). The RT-15 IRBM used the second and third stages of the RT-2 ICBM and was to be developed at TsKB-7 Arsenal in Leningrad under the direction of Pyotr A Tyurin. Both mobile and silo-based versions were designed. However work was stopped from 16 July 1963 to 25 December 1964 due to delays in development of the RT-2 on which the missile was based. Trials of the RT-15 using two 15P696 mobile launchers finally took place in 1965-1966. By that time the planned silo version was cancelled. The launcher was revealed publicly at the mammoth Moscow parade in 1967. TsKB-7 itself designed the first stage motors, with the solid propellant being developed by Vladimir S Shpak at GIPKh and produced by Yakov Savchenko at the Altaisk State Research Institute for Chemical Technology. Two variants of the second stage were developed in parallel. That flown on the first ten flights was developed by Mikhail Tsirulnikov at SKB-172 in Perm. The later variant was developed by the same team that produced the first stage. A variant using the Object 272 self-propelled-launcher based on the chassis of the T-10 tank was designed by Zh Ya Kotin at KB-3 at the Kirov Factory in Leningrad. The TTZ specification for this version was issued by GURVO on 24 September 1964. System integrator was V V Cherneskin at TsKB-34. A regiment of these launchers consisted of six launchers, one control vehicle, a MAZ-543 command vehicle, a position preparation vehicle, two diesel generators, and three 'Relef' communications/liaison vehicles. Trials were conducted at Kapustin Yar in 1965 to 1966 from launch areas 84 and 105. This version was paraded in Moscow in 1966. The complete mobile land-based launch complex (PBRK) underwent trials from November 1966 to March 1970. Twenty launches were made with this variant, including two dual salvo launches. Although series production was cancelled on 6 June 1969, it was recommended that an experimental regiment be formed to test the military utility of a mobile solid propellant missile. Some claim that this regiment went into service in Byelorussia in 1970 with 19 launchers of various types. Reportedly the Arsenal factory produced only 15 series RT-15's before production was ended. Maximum range: 2,500 km (1,500 mi). Number Standard Warheads: 1. Warhead yield: 50 KT. CEP: 2.26 km (1.40 mi). Boost Propulsion: Solid rocket. Initial Operational Capability: 1970. Total Number Built: 19. Subtopics RT-15M Russian submarine-launched ballistic missile. Under the original resolution in 1961 starting the RT-2 program, Makeyev was to develop a submarine-launched version of the RT-15, consisting of the first and second stages of the RT-2. It did not proceed beyond the study stage. Family: IRBM, vehicle-launched. Country: Russia. Launch Sites: Kapustin Yar, Kapustin Yar LC84, Kapustin Yar V-2. Stages: 15D94, 15D27. Agency: Arsenal. Bibliography: 2, 475, 476, 8553. Photo Gallery RT-15 1965 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1965 September 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC84. Launch Pad: LC84?. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). November 1966 - . Launch Site: Kapustin Yar. LV Family: RT-2. Launch Vehicle: RT-15. First RT-15 launch in regiment test series. - . Nation: Russia. Agency: RVSN. 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1970 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1970 March 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

The book retraces every stage in the history of a club that has survived wars, passed through glorious and inglorious moments, and lived through different historical eras.

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The new site, like the one that preceded it, has the objective of presenting this invaluable piece of history to a wider audience, granting it the visibility it truly deserves.

A variant using the Object 272 self-propelled-launcher based on the chassis of the T-10 tank was designed by Zh Ya Kotin at KB-3 at the Kirov Factory in Leningrad. The TTZ specification for this version was issued by GURVO on 24 September 1964. System integrator was V V Cherneskin at TsKB-34. A regiment of these launchers consisted of six launchers, one control vehicle, a MAZ-543 command vehicle, a position preparation vehicle, two diesel generators, and three 'Relef' communications/liaison vehicles. Trials were conducted at Kapustin Yar in 1965 to 1966 from launch areas 84 and 105. This version was paraded in Moscow in 1966. The complete mobile land-based launch complex (PBRK) underwent trials from November 1966 to March 1970. Twenty launches were made with this variant, including two dual salvo launches. Although series production was cancelled on 6 June 1969, it was recommended that an experimental regiment be formed to test the military utility of a mobile solid propellant missile. Some claim that this regiment went into service in Byelorussia in 1970 with 19 launchers of various types. Reportedly the Arsenal factory produced only 15 series RT-15's before production was ended. Maximum range: 2,500 km (1,500 mi). Number Standard Warheads: 1. Warhead yield: 50 KT. CEP: 2.26 km (1.40 mi). Boost Propulsion: Solid rocket. Initial Operational Capability: 1970. Total Number Built: 19. Subtopics RT-15M Russian submarine-launched ballistic missile. Under the original resolution in 1961 starting the RT-2 program, Makeyev was to develop a submarine-launched version of the RT-15, consisting of the first and second stages of the RT-2. It did not proceed beyond the study stage. Family: IRBM, vehicle-launched. Country: Russia. Launch Sites: Kapustin Yar, Kapustin Yar LC84, Kapustin Yar V-2. Stages: 15D94, 15D27. Agency: Arsenal. Bibliography: 2, 475, 476, 8553. Photo Gallery RT-15 1965 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1965 September 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC84. Launch Pad: LC84?. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). November 1966 - . Launch Site: Kapustin Yar. LV Family: RT-2. Launch Vehicle: RT-15. First RT-15 launch in regiment test series. - . Nation: Russia. Agency: RVSN. 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1970 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1970 March 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

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In rowing, the unforgettable successes of the 1930s and 1940s achieved by athletes such as Antonio Ghiardello, Giliante D’Este, Francesco Cossu and Antonio Provenzani, who clinched medals at the Los Angeles Olympics in 1932, along with Romolo Catasta, bronze medallist at the London Olympics in 1948, were followed by a sustained period of success.

So much water has passed under the bridges of the River Tiber since the four founders in a bohemian atmosphere gave life to our association, but the spirit that animates it remains unchanged and, thanks to this the Circolo Canottieri Aniene has renewed its bond with the city of Rome, with its sports disciplines, above all rowing and swimming.

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The long and glorious history of the Circolo Canottieri Aniene is told in Consocio Gianfranco Tobia’s book I Cento Anni del Circolo Canottieri Aniene (One hundred Years of the Circolo Canottieri Aniene).

Aniene’s multiple wins at international level, under the unparalleled leadership of Ghiardello, marked a veritable competitive explosion. Towards the 1950s, the club made a decisive choice towards its future, laying the foundations for the construction of the large complex that to this day constitutes our headquarters.

Trials of the RT-15 using two 15P696 mobile launchers finally took place in 1965-1966. By that time the planned silo version was cancelled. The launcher was revealed publicly at the mammoth Moscow parade in 1967. TsKB-7 itself designed the first stage motors, with the solid propellant being developed by Vladimir S Shpak at GIPKh and produced by Yakov Savchenko at the Altaisk State Research Institute for Chemical Technology. Two variants of the second stage were developed in parallel. That flown on the first ten flights was developed by Mikhail Tsirulnikov at SKB-172 in Perm. The later variant was developed by the same team that produced the first stage. A variant using the Object 272 self-propelled-launcher based on the chassis of the T-10 tank was designed by Zh Ya Kotin at KB-3 at the Kirov Factory in Leningrad. The TTZ specification for this version was issued by GURVO on 24 September 1964. System integrator was V V Cherneskin at TsKB-34. A regiment of these launchers consisted of six launchers, one control vehicle, a MAZ-543 command vehicle, a position preparation vehicle, two diesel generators, and three 'Relef' communications/liaison vehicles. Trials were conducted at Kapustin Yar in 1965 to 1966 from launch areas 84 and 105. This version was paraded in Moscow in 1966. The complete mobile land-based launch complex (PBRK) underwent trials from November 1966 to March 1970. Twenty launches were made with this variant, including two dual salvo launches. Although series production was cancelled on 6 June 1969, it was recommended that an experimental regiment be formed to test the military utility of a mobile solid propellant missile. Some claim that this regiment went into service in Byelorussia in 1970 with 19 launchers of various types. Reportedly the Arsenal factory produced only 15 series RT-15's before production was ended. Maximum range: 2,500 km (1,500 mi). Number Standard Warheads: 1. Warhead yield: 50 KT. CEP: 2.26 km (1.40 mi). Boost Propulsion: Solid rocket. Initial Operational Capability: 1970. Total Number Built: 19. Subtopics RT-15M Russian submarine-launched ballistic missile. Under the original resolution in 1961 starting the RT-2 program, Makeyev was to develop a submarine-launched version of the RT-15, consisting of the first and second stages of the RT-2. It did not proceed beyond the study stage. Family: IRBM, vehicle-launched. Country: Russia. Launch Sites: Kapustin Yar, Kapustin Yar LC84, Kapustin Yar V-2. Stages: 15D94, 15D27. Agency: Arsenal. Bibliography: 2, 475, 476, 8553. Photo Gallery RT-15 1965 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1965 September 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC84. Launch Pad: LC84?. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). November 1966 - . Launch Site: Kapustin Yar. LV Family: RT-2. Launch Vehicle: RT-15. First RT-15 launch in regiment test series. - . Nation: Russia. Agency: RVSN. 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1970 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1970 March 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

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Key Parameters of Band Pass Filters · Center Frequency (fC): This is the midpoint frequency between fL and fH. · Bandwidth (BW): This is the range of ...

Route15NJ accident today

Decree 316-157 of 4 April 1961 authorized development of a family of solid propellant launch vehicles utilizing various combinations of three stages (the RT-2, RT-15, and RT-25). The RT-15 IRBM used the second and third stages of the RT-2 ICBM and was to be developed at TsKB-7 Arsenal in Leningrad under the direction of Pyotr A Tyurin. Both mobile and silo-based versions were designed. However work was stopped from 16 July 1963 to 25 December 1964 due to delays in development of the RT-2 on which the missile was based. Trials of the RT-15 using two 15P696 mobile launchers finally took place in 1965-1966. By that time the planned silo version was cancelled. The launcher was revealed publicly at the mammoth Moscow parade in 1967. TsKB-7 itself designed the first stage motors, with the solid propellant being developed by Vladimir S Shpak at GIPKh and produced by Yakov Savchenko at the Altaisk State Research Institute for Chemical Technology. Two variants of the second stage were developed in parallel. That flown on the first ten flights was developed by Mikhail Tsirulnikov at SKB-172 in Perm. The later variant was developed by the same team that produced the first stage. A variant using the Object 272 self-propelled-launcher based on the chassis of the T-10 tank was designed by Zh Ya Kotin at KB-3 at the Kirov Factory in Leningrad. The TTZ specification for this version was issued by GURVO on 24 September 1964. System integrator was V V Cherneskin at TsKB-34. A regiment of these launchers consisted of six launchers, one control vehicle, a MAZ-543 command vehicle, a position preparation vehicle, two diesel generators, and three 'Relef' communications/liaison vehicles. Trials were conducted at Kapustin Yar in 1965 to 1966 from launch areas 84 and 105. This version was paraded in Moscow in 1966. The complete mobile land-based launch complex (PBRK) underwent trials from November 1966 to March 1970. Twenty launches were made with this variant, including two dual salvo launches. Although series production was cancelled on 6 June 1969, it was recommended that an experimental regiment be formed to test the military utility of a mobile solid propellant missile. Some claim that this regiment went into service in Byelorussia in 1970 with 19 launchers of various types. Reportedly the Arsenal factory produced only 15 series RT-15's before production was ended. Maximum range: 2,500 km (1,500 mi). Number Standard Warheads: 1. Warhead yield: 50 KT. CEP: 2.26 km (1.40 mi). Boost Propulsion: Solid rocket. Initial Operational Capability: 1970. Total Number Built: 19. Subtopics RT-15M Russian submarine-launched ballistic missile. Under the original resolution in 1961 starting the RT-2 program, Makeyev was to develop a submarine-launched version of the RT-15, consisting of the first and second stages of the RT-2. It did not proceed beyond the study stage. Family: IRBM, vehicle-launched. Country: Russia. Launch Sites: Kapustin Yar, Kapustin Yar LC84, Kapustin Yar V-2. Stages: 15D94, 15D27. Agency: Arsenal. Bibliography: 2, 475, 476, 8553. Photo Gallery RT-15 1965 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1965 September 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC84. Launch Pad: LC84?. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). November 1966 - . Launch Site: Kapustin Yar. LV Family: RT-2. Launch Vehicle: RT-15. First RT-15 launch in regiment test series. - . Nation: Russia. Agency: RVSN. 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1970 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1970 March 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

With the new course undertaken by the Circolo Canottieri Aniene with its move to Acqua Acetosa, further disciplines were added to rowing, which nevertheless remains the pride of our club. Indeed, over the years, tennis, five-a-side football, canoeing and swimming have also been introduced, sports in which we have become the leading Italian club in both men’s and women’s fields and consequently the winners of the national team championship.

The complete mobile land-based launch complex (PBRK) underwent trials from November 1966 to March 1970. Twenty launches were made with this variant, including two dual salvo launches. Although series production was cancelled on 6 June 1969, it was recommended that an experimental regiment be formed to test the military utility of a mobile solid propellant missile. Some claim that this regiment went into service in Byelorussia in 1970 with 19 launchers of various types. Reportedly the Arsenal factory produced only 15 series RT-15's before production was ended. Maximum range: 2,500 km (1,500 mi). Number Standard Warheads: 1. Warhead yield: 50 KT. CEP: 2.26 km (1.40 mi). Boost Propulsion: Solid rocket. Initial Operational Capability: 1970. Total Number Built: 19. Subtopics RT-15M Russian submarine-launched ballistic missile. Under the original resolution in 1961 starting the RT-2 program, Makeyev was to develop a submarine-launched version of the RT-15, consisting of the first and second stages of the RT-2. It did not proceed beyond the study stage. Family: IRBM, vehicle-launched. Country: Russia. Launch Sites: Kapustin Yar, Kapustin Yar LC84, Kapustin Yar V-2. Stages: 15D94, 15D27. Agency: Arsenal. Bibliography: 2, 475, 476, 8553. Photo Gallery RT-15 1965 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1965 September 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC84. Launch Pad: LC84?. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). November 1966 - . Launch Site: Kapustin Yar. LV Family: RT-2. Launch Vehicle: RT-15. First RT-15 launch in regiment test series. - . Nation: Russia. Agency: RVSN. 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1967 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1968 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1969 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1970 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). 1970 March 1 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: RT-2. Launch Vehicle: RT-15. Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use