B-611 vs R-36 (missile): Specs Compared

FORCETALLY

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ABallistic missiles

Short-range ballistic missile

BBallistic missiles

Intercontinental ballistic missile

First system

Second system

At a glance

B-611larger figure on 0 of 1

R-36 (missile)larger figure on 1 of 1

Counts only measures both sources give with the same scope. A larger figure is not a better system.

Measured figures

8 of 22 rows sourced on both sides

—

32.2m

Length

All recorded figures & sources

32.2 m

Length

Single source

18.9 m

R-36-O

Single source

Configuration

B-611 and R-36 (missile) configuration
Specification	B-611	R-36 (missile)
Type	Short-range ballistic missile^[source]	Intercontinental ballistic missile^[source]
Place of origin	China^[source]	Soviet Union^[source]
Used by	See § Operators^[source]	Russian Strategic Rocket Forces^[source]
Manufacturer	China Aerospace Science and Industry Corporation (CASIC)^[source]	Factory: Yuzhny Machine-Building Plant Developer: Yuzhnoye Design Office

Detonation mechanism	Proximity / impact^[source]	—

Engine	Solid fuel rocket motor^[source]	Two or three (R-36MUTTKH and R-36M2) liquid fueled rocket stages First Stage: 1x RD-251 (R-36) 1x RD-251P (R-36P) 1x RD-251M (R-36-O) 1x RD-264 (R-36M) 1x RD-264 (R-36MUTTKh and R-36M2) Second Stage: 1x RD-252 (R-36) 1x RD-252 (R-36P) 1x RD-0228 (R-36M) 1x RD-0255 (R-36MUTTKh) 1x RD-0255 (R-36M2) Third Stage: 1x RD-864 (R-36MUTTKh) 1x RD-869 (R-36M2)^[source]

Propellant	Solid fuel^[source]	N 2 O 4 / UDMH^[source]

Guidance system	Inertial and optical guidance systems^[source]	Inertial, autonomous^[source]

In service	—	1966–1979 (original variant) 1988–present (R-36M2 Voevoda variant)^[source]

Designed	—	From 1962^[source]

Unit cost	—	$7,000,000^[source]

Warhead	—	Depending on variant (see variants). Newest (R-36M2), 10 × 550–750 kiloton MIRV warheads with a large amount of decoys and other penetration aids . Originally (R-36), 1 × 8–20 megaton warhead.^[source]