|
R-16 |
R-16U | |
|---|---|---|
|
Launch platform |
Open-launch |
Open-launch, silo-based |
|
Reaction time from high alert condition, min |
18 |
|
|
Guaranteed time in a fueled state, days |
30 | |
|
Number of silo launchers in launch complex |
3 | |
8K64 and 8K64U (SS-7) Missiles
The 8K64 is the first two-stage intercontinental ballistic missile designed by OKB-586.
The main innovation was the use of swiveling chambers of the steering engines as controls.
The missile could be equipped with two types of nuclear payload: a “light” warhead to fire at a maximum range, and a “heavy” warhead with a heavier charge to hit protected facilities (targets).
307 missiles were launched in total, with 91% success rate.
8K64 and 8K64U Missile Basic Specifications
| 8K64 (8K64U) | |
|---|---|
|
Number of stages |
2 |
|
Launch weight, tnf |
140,6 |
|
Length, m |
34,3 |
|
Diameter, m |
3 |
|
Propellants: |
Liquid, high-boiling, hypergolic |
|
- oxidizer |
АK-27I |
|
- fuel |
UDMH |
|
Warhead, Mt |
2,3 (5,0) |
|
Maximum operational range, km |
13000 |
|
In service |
1962-1976 |
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