SLBM - R-29RM (3M37, 4K75RM, RSM-54, SS-N-23 Skiff)

Р-29РМ (3М37, 4К75РМ, РСМ-54)
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).
URL : https://www.valka.cz/SLBM-R-29RM-3M37-4K75RM-RSM-54-SS-N-23-Skiff-t21532#82289 Version : 0

This post has not been translated to English yet. Please use the TRANSLATE button above to see machine translation of this post.

foto z (www.globalsecurity.org)
URL : https://www.valka.cz/SLBM-R-29RM-3M37-4K75RM-RSM-54-SS-N-23-Skiff-t21532#87459 Version : 0
Discussion post Fact post
Attachments

Join us

We believe that there are people with different interests and experiences who could contribute their knowledge and ideas. If you love military history and have experience in historical research, writing articles, editing text, moderating, creating images, graphics or videos, or simply have a desire to contribute to our unique system, you can join us and help us create content that will be interesting and beneficial to other readers.

Find out more