LabLynx Wiki

LabLynx Wiki
RT-23
BZhRK three-car autonomous launching module
TypeICBM
Place of originUSSR
Service history
In service1987–2005[1]
Production history
ManufacturerYuzhnoye Design Bureau
Specifications
Mass104,500 kg (230,400 lb)
Length23,400 mm (920 in)
Diameter2,410 mm (95 in)
Warhead10 × 550 kt MIRVs[2]

EngineFirst stage: 15D305,[3]
Second stage: 15D339[3]
15D305: 3,040 kN,[4]
15D339: 1,470 kN[5]
PropellantSolid fuel
Operational
range
10,000–11,000 km (6,200–6,800 mi)[2]
Guidance
system
Inertial, autonomous
Accuracy150–500 m[2]
Launch
platform
Railcar TEL or silo

The RT-23 Molodets (Russian: РТ-23 УТТХ[6] «Мо́лодец», lit.

LIMSpec Wiki

LIMSpec Wiki
RT-23
BZhRK three-car autonomous launching module
TypeICBM
Place of originUSSR
Service history
In service1987–2005[1]
Production history
ManufacturerYuzhnoye Design Bureau
Specifications
Mass104,500 kg (230,400 lb)
Length23,400 mm (920 in)
Diameter2,410 mm (95 in)
Warhead10 × 550 kt MIRVs[2]

EngineFirst stage: 15D305,[3]
Second stage: 15D339[3]
15D305: 3,040 kN,[4]
15D339: 1,470 kN[5]
PropellantSolid fuel
Operational
range
10,000–11,000 km (6,200–6,800 mi)[2]
Guidance
system
Inertial, autonomous
Accuracy150–500 m[2]
Launch
platform
Railcar TEL or silo

The RT-23 Molodets (Russian: РТ-23 УТТХ[6] «Мо́лодец», lit.

Bioinformatics Wiki

Bioinformatics Wiki
RT-23
BZhRK three-car autonomous launching module
TypeICBM
Place of originUSSR
Service history
In service1987–2005[1]
Production history
ManufacturerYuzhnoye Design Bureau
Specifications
Mass104,500 kg (230,400 lb)
Length23,400 mm (920 in)
Diameter2,410 mm (95 in)
Warhead10 × 550 kt MIRVs[2]

EngineFirst stage: 15D305,[3]
Second stage: 15D339[3]
15D305: 3,040 kN,[4]
15D339: 1,470 kN[5]
PropellantSolid fuel
Operational
range
10,000–11,000 km (6,200–6,800 mi)[2]
Guidance
system
Inertial, autonomous
Accuracy150–500 m[2]
Launch
platform
Railcar TEL or silo

The RT-23 Molodets (Russian: РТ-23 УТТХ[6] «Мо́лодец», lit.

IHE Wiki

IHE Wiki
RT-23
BZhRK three-car autonomous launching module
TypeICBM
Place of originUSSR
Service history
In service1987–2005[1]
Production history
ManufacturerYuzhnoye Design Bureau
Specifications
Mass104,500 kg (230,400 lb)
Length23,400 mm (920 in)
Diameter2,410 mm (95 in)
Warhead10 × 550 kt MIRVs[2]

EngineFirst stage: 15D305,[3]
Second stage: 15D339[3]
15D305: 3,040 kN,[4]
15D339: 1,470 kN[5]
PropellantSolid fuel
Operational
range
10,000–11,000 km (6,200–6,800 mi)[2]
Guidance
system
Inertial, autonomous
Accuracy150–500 m[2]
Launch
platform
Railcar TEL or silo

The RT-23 Molodets (Russian: РТ-23 УТТХ[6] «Мо́лодец», lit.

HL7 Wiki

HL7 Wiki
RT-23
BZhRK three-car autonomous launching module
TypeICBM
Place of originUSSR
Service history
In service1987–2005[1]
Production history
ManufacturerYuzhnoye Design Bureau
Specifications
Mass104,500 kg (230,400 lb)
Length23,400 mm (920 in)
Diameter2,410 mm (95 in)
Warhead10 × 550 kt MIRVs[2]

EngineFirst stage: 15D305,[3]
Second stage: 15D339[3]
15D305: 3,040 kN,[4]
15D339: 1,470 kN[5]
PropellantSolid fuel
Operational
range
10,000–11,000 km (6,200–6,800 mi)[2]
Guidance
system
Inertial, autonomous
Accuracy150–500 m[2]
Launch
platform
Railcar TEL or silo

The RT-23 Molodets (Russian: РТ-23 УТТХ[6] «Мо́лодец», lit.

Clinfowiki

Clinfowiki
RT-23
BZhRK three-car autonomous launching module
TypeICBM
Place of originUSSR
Service history
In service1987–2005[1]
Production history
ManufacturerYuzhnoye Design Bureau
Specifications
Mass104,500 kg (230,400 lb)
Length23,400 mm (920 in)
Diameter2,410 mm (95 in)
Warhead10 × 550 kt MIRVs[2]

EngineFirst stage: 15D305,[3]
Second stage: 15D339[3]
15D305: 3,040 kN,[4]
15D339: 1,470 kN[5]
PropellantSolid fuel
Operational
range
10,000–11,000 km (6,200–6,800 mi)[2]
Guidance
system
Inertial, autonomous
Accuracy150–500 m[2]
Launch
platform
Railcar TEL or silo

The RT-23 Molodets (Russian: РТ-23 УТТХ[6] «Мо́лодец», lit.

OpenWetWare

OpenWetWare
RT-23
BZhRK three-car autonomous launching module
TypeICBM
Place of originUSSR
Service history
In service1987–2005[1]
Production history
ManufacturerYuzhnoye Design Bureau
Specifications
Mass104,500 kg (230,400 lb)
Length23,400 mm (920 in)
Diameter2,410 mm (95 in)
Warhead10 × 550 kt MIRVs[2]

EngineFirst stage: 15D305,[3]
Second stage: 15D339[3]
15D305: 3,040 kN,[4]
15D339: 1,470 kN[5]
PropellantSolid fuel
Operational
range
10,000–11,000 km (6,200–6,800 mi)[2]
Guidance
system
Inertial, autonomous
Accuracy150–500 m[2]
Launch
platform
Railcar TEL or silo

The RT-23 Molodets (Russian: РТ-23 УТТХ[6] «Мо́лодец», lit.

Statistical Genetics Wiki

Statistical Genetics Wiki
RT-23
BZhRK three-car autonomous launching module
TypeICBM
Place of originUSSR
Service history
In service1987–2005[1]
Production history
ManufacturerYuzhnoye Design Bureau
Specifications
Mass104,500 kg (230,400 lb)
Length23,400 mm (920 in)
Diameter2,410 mm (95 in)
Warhead10 × 550 kt MIRVs[2]

EngineFirst stage: 15D305,[3]
Second stage: 15D339[3]
15D305: 3,040 kN,[4]
15D339: 1,470 kN[5]
PropellantSolid fuel
Operational
range
10,000–11,000 km (6,200–6,800 mi)[2]
Guidance
system
Inertial, autonomous
Accuracy150–500 m[2]
Launch
platform
Railcar TEL or silo

The RT-23 Molodets (Russian: РТ-23 УТТХ[6] «Мо́лодец», lit.

Cloud-Standards.org

Cloud-Standards.org
RT-23
BZhRK three-car autonomous launching module
TypeICBM
Place of originUSSR
Service history
In service1987–2005[1]
Production history
ManufacturerYuzhnoye Design Bureau
Specifications
Mass104,500 kg (230,400 lb)
Length23,400 mm (920 in)
Diameter2,410 mm (95 in)
Warhead10 × 550 kt MIRVs[2]

EngineFirst stage: 15D305,[3]
Second stage: 15D339[3]
15D305: 3,040 kN,[4]
15D339: 1,470 kN[5]
PropellantSolid fuel
Operational
range
10,000–11,000 km (6,200–6,800 mi)[2]
Guidance
system
Inertial, autonomous
Accuracy150–500 m[2]
Launch
platform
Railcar TEL or silo

The RT-23 Molodets (Russian: РТ-23 УТТХ[6] «Мо́лодец», lit.

WikiBooks

WikiBooks
RT-23
BZhRK three-car autonomous launching module
TypeICBM
Place of originUSSR
Service history
In service1987–2005[1]
Production history
ManufacturerYuzhnoye Design Bureau
Specifications
Mass104,500 kg (230,400 lb)
Length23,400 mm (920 in)
Diameter2,410 mm (95 in)
Warhead10 × 550 kt MIRVs[2]

EngineFirst stage: 15D305,[3]
Second stage: 15D339[3]
15D305: 3,040 kN,[4]
15D339: 1,470 kN[5]
PropellantSolid fuel
Operational
range
10,000–11,000 km (6,200–6,800 mi)[2]
Guidance
system
Inertial, autonomous
Accuracy150–500 m[2]
Launch
platform
Railcar TEL or silo

The RT-23 Molodets (Russian: РТ-23 УТТХ[6] «Мо́лодец», lit.

LIMSwiki

LIMSwiki
RT-23
BZhRK three-car autonomous launching module
TypeICBM
Place of originUSSR
Service history
In service1987–2005[1]
Production history
ManufacturerYuzhnoye Design Bureau
Specifications
Mass104,500 kg (230,400 lb)
Length23,400 mm (920 in)
Diameter2,410 mm (95 in)
Warhead10 × 550 kt MIRVs[2]

EngineFirst stage: 15D305,[3]
Second stage: 15D339[3]
15D305: 3,040 kN,[4]
15D339: 1,470 kN[5]
PropellantSolid fuel
Operational
range
10,000–11,000 km (6,200–6,800 mi)[2]
Guidance
system
Inertial, autonomous
Accuracy150–500 m[2]
Launch
platform
Railcar TEL or silo

The RT-23 Molodets (Russian: РТ-23 УТТХ[6] «Мо́лодец», lit.

Wikiversity

Wikiversity
RT-23
BZhRK three-car autonomous launching module
TypeICBM
Place of originUSSR
Service history
In service1987–2005[1]
Production history
ManufacturerYuzhnoye Design Bureau
Specifications
Mass104,500 kg (230,400 lb)
Length23,400 mm (920 in)
Diameter2,410 mm (95 in)
Warhead10 × 550 kt MIRVs[2]

EngineFirst stage: 15D305,[3]
Second stage: 15D339[3]
15D305: 3,040 kN,[4]
15D339: 1,470 kN[5]
PropellantSolid fuel
Operational
range
10,000–11,000 km (6,200–6,800 mi)[2]
Guidance
system
Inertial, autonomous
Accuracy150–500 m[2]
Launch
platform
Railcar TEL or silo

The RT-23 Molodets (Russian: РТ-23 УТТХ[6] «Мо́лодец», lit.

Wikipedia

Wikipedia
RT-23
BZhRK three-car autonomous launching module
TypeICBM
Place of originUSSR
Service history
In service1987–2005[1]
Production history
ManufacturerYuzhnoye Design Bureau
Specifications
Mass104,500 kg (230,400 lb)
Length23,400 mm (920 in)
Diameter2,410 mm (95 in)
Warhead10 × 550 kt MIRVs[2]

EngineFirst stage: 15D305,[3]
Second stage: 15D339[3]
15D305: 3,040 kN,[4]
15D339: 1,470 kN[5]
PropellantSolid fuel
Operational
range
10,000–11,000 km (6,200–6,800 mi)[2]
Guidance
system
Inertial, autonomous
Accuracy150–500 m[2]
Launch
platform
Railcar TEL or silo

The RT-23 Molodets (Russian: РТ-23 УТТХ[6] «Мо́лодец», lit.