9S52 Polyana-D4 ASU Russian 6x6 Air Defense Command and Control Vehicle

9S52 Polyana-D4 ASU

Air-launched Cruise Missile (ALCM)

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9S52 Polyana-D4 ASU Russian 6x6 Air Defense Command and Control Vehicle — Polyana-D4_(A).jpgTRADOC ODIN WEG

Basic Information

Name

9S52 Polyana-D4 ASU Russian 6x6 Air Defense Command and Control Vehicle

Designation

9S52 Polyana-D4 ASU

Alternate Designation

9S52 Polyana-D4 ASU

Equipment Type

Air-launched Cruise Missile (ALCM)

Manufacturer

Scientific Research Institute of the automatization technics of Minradioprom

Date of Introduction

1986

Description

9S52 Polyana-D4 ASU is a Soviet/Russian automated command and control system for air defense troops. May act as an upper-level command post (CP) of the SAM brigade including S-300V as well as the 9K37 Buk complex. And also other means, including aircraft. Developed by Scientific Research Institute of the automatization technics of Minradioprom. Chief designer - G.A.Burlakov. Development works started under the Decisions of the Special Commission of the Presidium of the USSR Soviet Ministry on military-industrial questions dated June 29, 1977, and August 27, 1981. Mass production of the system was organized at the Minsk Electromechanical Plant (currently GNPO Agat), but later transferred to Penza, the former Minradioprom factory. In service since 1986. Chassis: Ural 375D

Ground Specifications

Mobility Type Wheeled (6x6)

Max Speed 75.0 km/h

Range 750.0 km

Variants

9S52M D4M Polyana system produced by Belarusian GNPO Agat, also developers of the Buk-MB modernisation of Buk-M1.

System

Alternate Designation 9S52 Polyana-D4 ASU

Type Air Defense Command and Control System

Chassis Ural 375

Composition Combat Control Post; COmmand-Staff Vehicle; Autonomous Automated Workstation; SPTA and Maintenance Trailer; Two ED1x30-T400-1RAM3 Mobile Electric Power Stations

Dimensions (Chassis: Ural 375D)

Height, Overall 2.68 m

Length, Overall 7.36 m

Width, Overall 2.67 m

Weight, Gross Vehicle 13.2 mt

Cargo Space (Chassis: Ural 375D)

Dimensions (Chassis: Ural 375D)

Length 3.9 m

Width 2.43 m

Height 0.872 m

Cargo Bed Area 9.5 m2

Automotive (Chassis: Ural 375D)

Engine Name ZiL-375 Diesel

Engine Type V8, 180 hp, Gasoline

Engine Power 180 hp

Cooling System Liquid

Fuel Capacity , Aux 60.0 liters

Fuel Capacity, Main Tank 300.0 liters

Maximum Road Speed 75 km/h

Maximum Range 750 km

Towing Capability, Off-Highway 5000.0 kg

Towing Capability, Off-Highway 10000.0 kg

Gradient 65 %

Side Slope 40 %

Vertical Step 0.8 m

Trench 0.7 m

Fording 1.2 m

Command and Control, Communication Equipment

Number of Interfaces with Superior CPs 1 ea

Number of Interfaces with Radar Data Sources up to 3

Number of Air Targets Tracked Simultaneously up to 250

Automated Workstation in CCP 8 ea

Automated Workstation in CSV 3 ea

Data Transfer Channels in CCP 16 ea

Data Transfer Channels in CSV 4 ea

Continuous Operation Time not less than 72 hours

Into/Out-of-Action Time Not more than 35 min

Radar Data Gathering and Processing Yes

Air Situation Monitoring Yes

Ground Situation Data Yes, receiving, gathering, and processing

Automated Data Registration and Recording Yes

Ciphering Equipment Capable Yes

Operating Temperature -40 deg C to +50 deg C

Image Sources

Notes https://en.m.wikipedia.org/wiki/File:Command_post_%22MP-06%22.jpg; https://www.ausairpower.net/APA-Rus-ADCP-CP.html;

Details

Country of Origin Russia

Category Land

Land

Classification

Domain

Ground

Equipment Status

Active

Dimensions

Length

7.36 m

Width

2.67 m

Height

2.68 m

Weight

13200 kg

Operators (1)

Russia

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