Ballistic missile 9M723 "Iskander-M"
Active radar homing head (ARLGSN) 9B918
Manufacturer: NPP RADAR MMS JSC
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9E436 optical correlation homing head
Manufacturer: TSNIIAG JSC
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9N730 cassette munition
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9N722K5 cassette warhead
Manufacturer: GOSNIIMASH JSC
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Receiving and processing unit of a satellite navigation system "Kometa-MR4-01"
Manufacturer: VNIIR-PROGRESS JSC
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Platformless inertial navigation system 9B918
Manufacturer: NII POLUS NAMED AFTER M.F. STELMAKH JSC
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MT-501-B laser gyroscope
Manufacturer: NII POLUS NAMED AFTER M.F. STELMAKH JSC
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BNP-B onboard navigation device with Baget-83V BCM
Manufacturer: KB KORUND-M JSC
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9H820 solid fuel engine (front wall)
Manufacturer: FNPC ALTAI JSC
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Antenna for the Kometa-MR4-01 satellite navigation system ARP-4T
Manufacturer: VNIIR-PROGRESS JSC
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9B899 false targets (system 200, or C200 A1-2 A1-3 UG2 UG3, or M51304)
Manufacturer: TSNIRTI NAMED AKADEMIKA A.I. BERGA JSC
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Receiving and processing unit of the BNA-B 9B919 satellite navigation system for MA2B
Manufacturer: NII KP JSC
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MA2B old-type satellite navigation system antenna
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MP-1.1S electric motor
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Automatic control unit
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Engine nozzle and rear wall 9X820 01.30.120
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Block of thermal batteries 04.20.000 - 9B283
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High-explosive warhead (9N722F, 9N722F1, 9N722F2, 9N722F3, A2G3 AA106)
Manufacturer: GOSNIIMASH JSC
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On-board control device (PUB) IRCU 469178.007
Manufacturer: PZTP CJSC
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Block of thermal batteries 04.20.000 - 9B283
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Cable network for power supply and information exchange LPI-A, LPI-UA 1.01.40.020.01 1.01.40.020.02
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Cable network for power supply and information exchange LPI-A, LPI-UA 1.01.40.020.01 1.01.40.020.02
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Antenna of the Kometa-R8 satellite navigation system ARP-4T
Manufacturer: VNIIR-PROGRESS JSC
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Steering blocks 9B915 (4 pcs.)
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Receiver 05.04.000
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Gas generator unit
Manufacturer: FNPC NII PRIKLADNOI KHIMII JSC
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Balloon of the 9M723.05.11.000 orientation and stabilisation system
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Aerodynamic steering wheel 9M723.04.04.000
Manufacturer: GKNPC M.V. KHRUNICHEV JSC
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Receiving and processing unit of the Kometa-R8 satellite navigation system
Manufacturer: VNIIR-PROGRESS JSC
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Specifications
| Length | 7 200 mm |
| Weight of the warhead | 410±10, 610±15 kg (depending on the warhead) |
| Launch weight | 3 800 kg |
| Types of warheads | cassette, fragmentation-high explosive, high explosive, penetrating, special (nuclear) |
| Maximum flight altitude | 100 km |
| Housing diameter | 920 mm |
| Type of trajectory | aeroballistic |
| Range | 500 km |
| Circular probable deviation | w/o homing head - 30-70 m, w/ homing head - 5-7 m |
| Speed near target | 700 - 800 m/sec |
| Maximum speed at the beginning of the final section | 2 600 m/sec |
| Speed at the end of the active section | 2 100 m/sec |
| Average flight altitude | 5 km |
| Set-up/take down time (with antenna devices) | up to 30 min |
| Flight mission calculation time | up to 10 sec |
| Interval between launches | up to 1 min |
| Launch time of the first missile from high readiness | up to 4 min |
| Time of launch of the first missile from the march | up to 6 min |
Total: 34
