Intercontinental ballistic missile. IOC: 2007. Country: Russia. Status: Active. Other Designations: RSM-56. Department of Defence Designation: SS-NX-30. Alternate Designation: Mace. Launch System: D-19M. Missile: 3M30. Solid-propellant Soviet intercontinental-range ballistic missile, equipped with multiple independently targeted warheads.
The first post-Soviet Russian ballistic missile, which will provide Russia's submarine-launched deterrent by the third decade of the 21st Century. Twelve Bulava missiles, each with as many as ten warheads, will be installed in each of six of the new Mark 955 Borei-class nuclear ballistic missile submarines.
Development of the Bulava missile began in 1999. Originally a different new solid-propellant missile was developed to that would fit in the existing R-39 missile tubes of the Typhoon-class submarines. The keel of the first Project 955 submarine, the Yuri Dolgoruky, was laid down at the Severodvinsk Nuclear Shipbuilding Centre in Arkhangelsk in 1996, and was to have entered service in 2001, replacing earlier Project 941 Typhoon-class ballistic missile submarines equipped with R-39 missiles. However the new solid-propellant ballistic missile failed in all three of its initial development tests in the late 1990's. That missile was cancelled and the Moscow Heat Engineering Institute was ordered to develop a new missile, the Bulava, in its place. The Yuri Dolgoruky, already in construction, had to be redesigned. The Typhoon-class SSBN selected for testing the Bulava, the Dmitry Donskoi, had to be heavily modified to Project 941UM standard. All of this resulted in the first test of the new missile being delayed to 2005, over seven years late to the original schedule.
In February 2004 President Putin claimed that the Bulava MIRV warheads could breach any available or potential anti-ballistic missile system. This presumably meant that they can maneuver after separation from the warhead bus, either in space or during reentry or both. Russia's Navy expected to commission the Yuri Dolgorukiy by 2006 and take delivery of at least two other submarines of the class by 2010. The keel of the second Mk 955, the Alexander Nevskiy was laid March 19, 2004 at the Sevmashpredpriyatiye shipyard.
The Bulava missile is significantly smaller than the R-39 series -- in fact, it is more like a solid-fuel replacement for the R-29 series. With a mass similar to the Minuteman 3, it would have an intercontinental throw weight of over a tonne. This in turn meant that its stated capability to carry as many as ten warheads could only be accomplished at ranges of around 7000 to 8000 km. Russian officials have reported that land-mobile versions of the missile will also be developed.
Official Characteristics as declared under START-2 Treaty:
Length of assembled missile without front section: 11.5 m
Maximum diameter of missile airframe (without stabilizers, raceways, protruding elements): 2.00 m
Launch weight: 36.8 tonnes
Total length of missile as a unit with launch canister (with front section): 12.1 m
Length of launch canister body. m: 12.1 m
Diameter of launch canister body (without protruding elements): 2.1 m
First stage:
- Stage length: 3.8 m
- Stage diameter: 2.00 m
- Weight of fully loaded stage: 18.6 tonnes
Second stage diameter: 2.00 m
Third stage diameter: 2.00 m
Official Characteristics as declared under START-2 Treaty:
Number of stages: 3
Length of assembled missile without front section: 17.9 m
Maximum diameter of missile airframe (without stabilizers, raceways, protruding elements): 1.86 m
Launch weight: 47.2 tonnes
Total length of missile as a unit with launch canister (with front section): 22.7 m
Total length of missile as a unit with launch canister (without front section): 19.4 m
Length of launch canister body: 19.4 m
Diameter of launch canister body (without protruding elements): 1.95 m
First stage:
- Stage length: 8.04 m
- Stage diameter: 1.86 m
- Weight of fully loaded stage: 28.6 tonnes
Second stage diameter: 1.61 m
Third stage diameter: 1.58 m
Manufacturer: MITT. Launches: 9. Failures: 4. Success Rate: 55.56%. First Launch Date: 2004-09-23. Last Launch Date: 2007-11-10. Launch data is: continuing. Apogee: 1,000 km (600 mi). Liftoff Thrust: 0 N ( lbf). Total Mass: 36,800 kg (81,100 lb). Core Diameter: 2.00 m (6.50 ft). Total Length: 12.10 m (39.60 ft). Maximum range: 10,500 km (6,500 mi). Number Standard Warheads: 10. Boost Propulsion: Solid rocket. Cruise Propulsion: Solid rocket. Stage 3 Propellants: Solid rocket. Guidance: Inertial + Stellar.
- Stage1: 1 x Topol'-M-1. Gross Mass: 26,000 kg (57,000 lb). Empty Mass: 3,000 kg (6,600 lb). Motor: 1 x 15Zh58A. Thrust (vac): 980.000 kN (220,310 lbf). Burn time: 60 sec. Length: 8.50 m (27.80 ft). Diameter: 1.80 m (5.90 ft). Propellants: Solid.
- Stage2: 1 x Topol'-M-2. Gross Mass: 13,000 kg (28,000 lb). Empty Mass: 1,500 kg (3,300 lb). Motor: 1 x 15Zh58B. Thrust (vac): 490.000 kN (110,150 lbf). Burn time: 64 sec. Length: 6.00 m (19.60 ft). Diameter: 1.55 m (5.08 ft). Propellants: Solid.
- Stage3: 1 x Topol'-M-3. Gross Mass: 6,000 kg (13,200 lb). Empty Mass: 1,000 kg (2,200 lb). Motor: 1 x 15Zh58V. Thrust (vac): 245.000 kN (55,078 lbf). Burn time: 56 sec. Length: 3.10 m (10.10 ft). Diameter: 1.34 m (4.39 ft). Propellants: Solid.
Bulava Chronology
2004 September 23 - Barents Sea Launch Area -. Bulava cold-launch test Agency: VMF. Apogee: 1.00 km (0.60 mi). Test of naval version of Topol M ICBM. A mass replica of a the new Bulava SLBM reached under 100 m altitude after being launched from the submerged SSBN Dmitry Donskoi.
2004 December 11 - Barents Sea Launch Area -. Bulava cold-launch test Agency: VMF. Apogee: 1.00 km (0.60 mi). A mass replica of a the new Bulava SLBM was ejected from its launch tube from the surfaced SSBN Dmitry Donskoi.
2005 September 27 - 13:22 GMT - White Sea Launch Area -. Bulava SLBM first flight. Agency: RVSN RF. Apogee: 1,000 km (600 mi). SLBM Development - first flight of new SLBM. Launched from TK-208 Dmitry Donskoy in the White Sea Launch Area.
2005 December 21 - 05:19 GMT - White Sea Launch Area -. Bulava SLBM test Agency: RVSN RF. Apogee: 1,000 km (600 mi). First submerged launch of the Bulava SLBM. Hit the designated impact area at Kura in the Kamchatka Peninsula.
2006 September 7 - 15:50 GMT - White Sea Launch Area -. FAILURE: Failure. Bulava SLBM test Agency: VMF. Apogee: 1.00 km (0.60 mi).
2006 October 25 - 13:05 GMT - White Sea Launch Area -. FAILURE: Failure. Bulava SLBM test Agency: VMF. Apogee: 100 km (60 mi).
2006 December 24 - White Sea Launch Area -. FAILURE: Failure. Agency: VMF. Apogee: 1.00 km (0.60 mi).
2007 June 28 - White Sea Launch Area -. Bulava SLBM test Agency: VMF. Apogee: 1,000 km (600 mi). The warhead impacted on target in the Kamchatka Peninsula. This was the first successful launch after two consecutive failures.
2007 November 10 - White Sea Launch Area -. FAILURE: Failure. Agency: VMF. Apogee: 1.00 km (0.60 mi).
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