Fattah-2 vs R-36 (missile): Specs Compared

FORCETALLY

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ABallistic missiles

Hypersonic missile

Credit

Unknown author Unknown author · CC BY 2.5 · Resized · CC BY 2.5 · Source ↗ · Modified

BBallistic missiles

Intercontinental ballistic missile

First system

Second system

At a glance

Fattah-2larger 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

7 of 20 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

Fattah-2 and R-36 (missile) configuration
Specification	Fattah-2	R-36 (missile)
Type	Hypersonic missile^[source]	Intercontinental ballistic missile^[source]
Used by	Iran^[source]	Russian Strategic Rocket Forces^[source]
Designer	IRGC engineers^[source]	—
Manufacturer	AIO^[source]	Factory: Yuzhny Machine-Building Plant Developer: Yuzhnoye Design Office^[source]
Warhead

Propellant	Stage 1: Solid‑Fuel Booster Stage 2: Liquid‑Fuel HGV^[source]	N 2 O 4 / UDMH^[source]

Launch platform	Road‑mobile TEL^[source]	Silo^[source]

Country of origin	Iran^[source] Iran^[source]	—

Place of origin	—	Soviet Union^[source]

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

Designed	—	From 1962^[source]

Unit cost	—	$7,000,000^[source]

Engine	—	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]