R-29RM, 3M37, RSM-54, SS-N-23 Skiff
Basic data
Missile system D-9RM, 16 missiles
Submarine: the Project 667BDRM
The beginning of the development: 1979
Design bureau: KBM (Engineering design office)
Manufacturer:
Flight test:
from June 1983 (on the ground)
Entry into service: 1986
Number of degrees: 3
Propulsion: storable liquid propellants
Firing sequence: under the sea from the flooded tube, on the surface of the
The number of warheads and power:
4 MIRV, tested MIRV 10 100 kt
Combat load: 2800 kg
Maximum range: 8300 km
Guidance: inertial with full stellar correction, uses satellite navigation
Accuracy: CEP 500 m
Length: 14.8 m
Maximum diameter: 1.90 m
Starting weight: 40.3 t
Oxidizer: nitrogen tetroxide
Fuel: unbalanced dimetylhyrazine (UDMH)
Source: Russian Strategic Nuclear Forces, Pavel Podvig, Oleg Bukharin, MIT Press, Cambridge, 2001
(original: Raketnije troops strategičeskogo naznačenija).
Basic data
Missile system D-9RM, 16 missiles
Submarine: the Project 667BDRM
The beginning of the development: 1979
Design bureau: KBM (Engineering design office)
Manufacturer:
Flight test:
from June 1983 (on the ground)
Entry into service: 1986
Number of degrees: 3
Propulsion: storable liquid propellants
Firing sequence: under the sea from the flooded tube, on the surface of the
The number of warheads and power:
4 MIRV, tested MIRV 10 100 kt
Combat load: 2800 kg
Maximum range: 8300 km
Guidance: inertial with full stellar correction, uses satellite navigation
Accuracy: CEP 500 m
Length: 14.8 m
Maximum diameter: 1.90 m
Starting weight: 40.3 t
Oxidizer: nitrogen tetroxide
Fuel: unbalanced dimetylhyrazine (UDMH)
Source: Russian Strategic Nuclear Forces, Pavel Podvig, Oleg Bukharin, MIT Press, Cambridge, 2001
(original: Raketnije troops strategičeskogo naznačenija).