Encyclopedia Astronautica
MR-UR-100



mrur100.gif
MR-UR-100
Credit: © Mark Wade
Ukrainian intercontinental ballistic missile. The Yangel MR-UR-100 was designed as a replacement for Chelomei's UR-100 at the end of its 10 year storage life. Although it could be installed in the same silos, it was 50% heavier. The competing design of Chelomei, the UR-100N, was also put into production when the Soviet hierarchy deadlocked and could not pick one design over the other.

The MR-UR-100 was Yangel's second attempt to get into production a competitor to Chelomei's UR-100 light ICBM. Design work began in 1964 after the R-36 had begun flight testing, thereby eliminating the leadership's grounds for prohibiting Yangel from working on the R-38. The concept was an ICBM to replace the UR-100 after it had exceeded its guaranteed storage life. Yangel envisioned a missile that would fit into the 15P084 missile silos built for the UR-100, but be heavier through use of a missile of maximum possible diameter. In order to allow this and permit the possibility of rapid reload, a gas generator was used to 'cold launch' the missile clear of the silo before the first stage engine ignited. The resulting payload increase would allow the missile to carry multiple independently-targeted warheads (MIRV's). Chelomei also proposed the larger UR-100N as a replacement, but launched using the traditional and less-expensive hot-launch technique.

The competition between the two chief designers led to a drama universally remarked upon in memoirs of Soviet rocketeers. Both design bureaux had powerful supporters in the Soviet leadership, and no consensus could be reached on which missile to put into production. The Yuzhnoye design was supported by Central Committee Secretary Ustinov, head of the VPK Military-Industrial Commission Smirnov, Mozhorin (Director of TNIIM), Tyulin (Deputy Commander MOM), and designers Glushko, and Pilyugin. Chelomei was supported by Marshal Grechko, Head of MOM Afanasyev, and designers Sergeyev, Barmin, Baryshev and V Kuznetsov.

Keldysh headed an expert commission to select a design, but the split within the technical community resulted in a deadlock. Premier Brezhnev finally made the Solomonic but extremely expensive decision at a leadership meeting at Stalin's old dacha at Yalta -- both would be built and deployed.

On 2 September 1969 a decree instructed KB Yuzhnoye to proceed with full development of the missile. The technical project was completed in 1969, with Utkin as the chief designer at Yuzhnoye.

The draft project for Glushko's RD-268 booster engine was completed in 1970. This was to be an upgrade of the RD-263 building-block of the R-36M's first stage. First engine tests were begun in March 1971.

In September 1970 MOM decreed that the missile must use a new 15P715P hardened silo design. This SM-SP-30 modification to the 15P084 silos was designed by TsKB-34 KBEM. It provided improved hardening against nearby nuclear detonations. The advanced project and a full-size mock-up for the modification had been completed in 1968. The design used shock absorbers and a container made of a special resin to allow the missile to survive in nearly every case unless the silo was in the crater of the enemy warhead explosion. The extra survivability came at a price -- conversion of a silo to use the MR-UR-100 cost three times more than converting it to use the UR-100N. Accordingly the MR-UR-100 would be deployed in only 1/7 the number of silos as its competitor.

Ground tests of the missile began in May 1971 at the Pavlograd Mechanical Factory, and began at Baikonur on 15 September 1972. For flight tests KBTM designed the 8P867 common pad facility that could be used with either the MR-UR-100 or R-36M. This was built as LC-67 at Tyuratam in 1970-1971, with the missile preparation facility being built at Area 42. A series of 30 trials launches were conducted from these pads and prototype silos from 26 December 1972 to 17 December 1974.

An official resolution was issued in October 1974 for the Yuzhnoye missile to go into production, although the work had already started a year earlier in anticipation of the decision. The missile was deployed in ten silos and one command point per regiment and the first regiment was already operational on 6 May 1975 at Vypolzovo. The missile was officially accepted for military service on 30 December 1975.

Deployment increased to 50 silos by the end of 1977, 100 by the end of 1978, and the final total of 150 in 1979. The missile was deployed in two fields at Bologoye and Kostroma. Only those missiles deployed after 11 November 1976 at Bologoye were emplaced in the superhardened silos. A training facility for missile crews was established at Belabanovo.

In 1979, during operational tests of missiles in-service, a problem was found with a high-frequency oscillation in the first stage motors. This severely degraded the missile's actual accuracy. Trials were made of modifications to fix the situation at the Perm Motor Machinery Factory between April and November 1977 under the direction of Ya M Sverdlov. The modification that solved the problem was officially accepted on 19 August 1980. It is not clear if the modification was made to field missiles, but the original model seems to have been replaced prematurely by its successor, the MR-UR-100UTTKh. Removal of MR-UR-100's from silos began in 1982 and all 150 were gone by the end of 1984.

The post-boost re-entry vehicle bus was separated from the missile's second stage by a solid propellant motor. It could be used to deliver a single warhead or dispense four warheads against separate targets. It also deployed countermeasures (decoys, jammers) to confuse enemy defences. The 71.1 tonne missile was fuelled with 63.2 tonnes of N2O4/UDMH storable propellants and had a guaranteed life of ten years, fuelled and ready to launch in its container within the silo.

Failures: 8. Success Rate: 91.84%. First Fail Date: 1971-12-10. Last Fail Date: 1982-01-28. Launch data is: incomplete. Standard warhead: 2,550 kg (5,620 lb). Maximum range: 10,320 km (6,410 mi). Number Standard Warheads: 1. Warhead yield: 3,600 KT. CEP: 0.45 km (0.27 mi). Alternate warhead: 2,600 kg (5,700 lb). Maximum range with alternate warhead: 10,200 km (6,300 mi). Number Alternate Warheads: 4. Alternate warhead yield: 300 KT. Alternate warhead CEP: 0.45 km (0.27 mi). Boost Propulsion: Storable liquid rocket, N2O4/UDMH. Cruise Thrust: 142.627 kN (32,064 lbf). Cruise Thrust: 14,544 kgf. Cruise engine: RD-862. Initial Operational Capability: 1975. Total Number Built: 50.

AKA: RS-16; MR-UR-100; SS-17 Mod 1 and Mod 2; 15A15; Spanker; 15P015.
Status: Retired 1988.
Gross mass: 71,100 kg (156,700 lb).
Payload: 2,550 kg (5,620 lb).
Height: 23.90 m (78.40 ft).
Diameter: 2.25 m (7.38 ft).
Span: 2.25 m (7.38 ft).
Thrust: 1,147.00 kN (257,855 lbf).
Apogee: 1,000 km (600 mi).
First Launch: 1971.12.10.
Last Launch: 1984.01.01.
Number: 64 .

More... - Chronology...


Associated Countries
Associated Engines
  • RD-268 Glushko N2O4/UDMH rocket engine. 1236 kN. MR-UR-100 / RS-16 (SS-17) stage 1. Out of Production. First flight 1976. Modification of RD-263 engine. Isp=319s. First flight 1990. More...
  • RD-862 Yuzhnoye N2O4/UDMH rocket engine. 142.630 kN. MR-UR-100 / RS-16 (SS-17) stage 2. Out of Production. Based on RD-857. Thrust vector control by secondary gas injection into nozzle. Roll control via special small jet nozzles. Isp=331s. More...
  • RD-863 Yuzhnoye N2O4/UDMH rocket engine. 276.840 kN. MR-UR-100 / RS-16 (SS-17) stage 1 attitude control engine. Out of Production. Isp=301s. More...

See also
  • MR-UR-100 The Yangel MR-UR-100 was designed as a replacement for Chelomei's UR-100 at the end of its 10 year storage life. Although it could be installed in the same silos, it was 50% heavier. The competing design of Chelomei, the UR-100N, was also put into production when the Soviet hierarchy deadlocked and could not pick one design over the other. More...
  • missile Guided self-propelled military weapon (as opposed to rocket, an unguided self-propelled weapon). More...

Associated Manufacturers and Agencies
  • Yuzhnoye Ukrainian manufacturer of rockets, spacecraft, and rocket engines. Yangel Design Bureau, Dnepropetrovsk, Ukraine. More...

Bibliography
  • McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: here.
  • Pervov, Mikhail, Raketnoye Oruzhiye RVSN, Violanta, Moscow, 1999..
  • Karpenko, A V, Utkin, A F and Popov,A D, Otechestvenniye strategischeskiye raketnoye kompleks, Sankt-Peterburg: Nevskii bastion; Gangut 1999..

Associated Launch Sites
  • Baikonur Russia's largest cosmodrome, the only one used for manned launches and with facilities for the larger Proton, N1, and Energia launch vehicles. The spaceport ended up on foreign soil after the break-up of Soviet Union. The official designations NIIP-5 and GIK-5 are used in official Soviet histories. It was also universally referred to as Tyuratam by both Soviet military staff and engineers, and the US intelligence agencies. Since the dissolution of the Soviet Union the Russian Federation has insisted on continued use of the old Soviet 'public' name of Baikonur. In its Kazakh (Kazak) version this is rendered Baykonur. More...

Associated Stages
  • MR-UR-100 St 1 N2O4/UDMH rocket stage. 1236.00 kN (277,864 lbf) thrust. Mass 59,000 kg (130,073 lb). More...
  • MR-UR-100-2 N2O4/UDMH rocket stage. 142.00 kN (31,923 lbf) thrust. Mass 10,000 kg (22,046 lb). More...

MR-UR-100 Chronology


1971 December 10 - . Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100. FAILURE: Failure.
  • BI-2 - . Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

1972 February 21 - . Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • BI-2 - . Nation: USSR. Agency: RVSN. Apogee: 1.00 km (0.60 mi).

1972 March 21 - . Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • BI-2 - . Nation: USSR. Agency: RVSN. Apogee: 1.00 km (0.60 mi).

1972 May 6 - . Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • BI-3 - . Nation: USSR. Agency: RVSN. Apogee: 10 km (6 mi).

1972 May 24 - . Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • BI-3 - . Nation: USSR. Agency: RVSN. Apogee: 10 km (6 mi).

1972 June 15 - . Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • BI-3 - . Nation: USSR. Agency: RVSN. Apogee: 10 km (6 mi).

1972 September 15 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • BI-4 - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1972 November 3 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • BI-4 - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1972 December 22 - . Launch Site: Baikonur. Launch Complex: Baikonur LC67/21. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • BI-2 - . Nation: USSR. Agency: RVSN. Apogee: 1.00 km (0.60 mi).

1972 December 26 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • BI-4 - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973 March 12 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973 April 6 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973 June 5 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100. FAILURE: Failure.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

1973 June 21 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973 July 9 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973 July 25 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973 October 2 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973 October 18 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973 November 4 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973 December 21 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973 December 27 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 February 4 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 February 26 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 March 1 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 April 3 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 April 27 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 April 28 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 May 28 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 May 31 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 June 21 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 August 28 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 September 14 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 September 27 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 October 22 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 October 23 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 November 12 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Operational test launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 December 17 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Mod 2 state trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1975 April 23 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Operational test launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1975 June 13 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1975 July 1 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1975 August 12 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1975 August 12 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1976 March 12 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials flight - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1976 May 17 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials flight - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1976 June 15 - . Launch Site: Baikonur. Launch Complex: Baikonur LC170. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1976 June 26 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1976 June 29 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Joint flight trials launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1976 August 12 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Operational test launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1976 October 21 - . Launch Site: Baikonur. Launch Complex: Baikonur LC170. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100. FAILURE: Failure.
  • Joint flight trials launch - . Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

1976 October 26 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Joint flight trials launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1976 December 14 - . Launch Site: Baikonur. Launch Complex: Baikonur LC170. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Joint flight trials launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1976 December 16 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Joint flight trials launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1976 December 30 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100. FAILURE: Failure.
  • Joint flight trials launch - . Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

1977 March 26 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Operational test launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1977 April 14 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Joint flight trials launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1977 May 25 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • K? - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1977 June 30 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Operational test launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1977 July 30 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Joint flight trials launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1978 February 27 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Operational missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1978 March 26 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Operational missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1978 June 5 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Operational missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1978 August 11 - . Launch Site: Baikonur. Launch Complex: Baikonur LC173. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Combat training launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1980 - . Launch Site: Baikonur. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Operational missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1984 - . Launch Site: Baikonur. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Operational missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

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