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MICH 2000

Facts from open sources (OSINT), each linked to its post or document; translated from Russian by a language model.

Specifications

ParameterValueSourcesWhere
Payload / warheadfrom 25 to 60 kg×7@warhistoryalconafter, @VictoryDrones, @uav_tech +4
Rangeup to 2000 km×6@texBPLA, @warhistoryalconafter, @VictoryDrones +3
Rangefrom 600 to 2000 km×4@DniproOfficial, @payloadUAV, @kcpn2014 +1
Cost48000 (basic configuration); +20000–25000 with CRPA antenna USD×4@uav_tech, @kcpn2014, @warhistoryalconafter +1
Costfrom 48 thousand USD×4@DniproOfficial, @texBPLA, @payloadUAV +1
modifications8 different modifications in "middle-strike" and "deep-strike" configurations×4@kcpn2014, @mil_hub, @payloadUAV +1
in_service_sinceautumn 2024×3@texBPLA, @payloadUAV, @mil_hub
localization85%, drops to 55% with CRPA installed %×3@payloadUAV, @mil_hub, @kcpn2014
Payload / warheadfrom 20 to 60 kg×2@DniproOfficial, @kcpn2014
base_platformChinese ZTK-150×2@payloadUAV, @mil_hub
control_channelsanalog radio link, digital, Starlink×2@payloadUAV, @mil_hub
distinguishing_featureforward canards (absent on Shahed-136)×2@payloadUAV, @mil_hub
navigationmulti-channel CRPA antenna (procured abroad)×2@payloadUAV, @mil_hub
operatorSBU "Alpha" unit×2@warhistoryalconafter, @DniproOfficial
variants8 variants, long-range version and medium-strike version×2@warhistoryalconafter, @uav_tech
Speed180–200 km/h ≠ sources disagree×1@kcpn2014
Speed≈ 150 km/h ≠ sources disagree×1@third_svitova
Gross weightseveral hundred×1@kcpn2014
Payload / warheadup to 60 kg×1@texBPLA
Dimensionslength and wingspan ~2.5–3 m×1@kcpn2014
appearanceShahed-like (resembling a Shahed)×1@milinua
colorblack and grey body×1@texBPLA
commsradio, digital link or Starlink — optional×1@kcpn2014
communicationradio, digital or Starlink — operator's choice×1@DniproOfficial
cost_with_crpa68000–73000 USD×1@VictoryDrones
design_notehas forward horizontal stabilizers, externally similar to Shahed-136/Geran-2×1@uav_tech
development_startlate 2023×1@DniproOfficial
engine_positioninternal combustion engine in the tail×1@kcpn2014
first_use_dateOctober 2024×1@uav_tech
guidancemid-course guidance, Starlink installation option×1@warhistoryalconafter
launchfrom ground rail, solid-fuel booster acceleration×1@kcpn2014
launch_platformfixed ground launcher×1@mil_hub
layouthybrid: tailless ("flying wing") plus forward horizontal stabilizer (canard), delta wing, wingtip fins×1@kcpn2014
localization_level85 %×1@texBPLA
modificationseight different modifications in "middle-strike" and "deep-strike" configurations×1@DniproOfficial
navigationautopilot + satellite + inertial navigation, Starlink optional×1@kcpn2014
operating_unitSBU "Alpha" Special Operations Center×1@payloadUAV
operatorSBU "Alpha" Special Operations Center×1@mil_hub
origindeveloped from the Chinese ZTK-150 prototype, external appearance retained, internals changed×1@DniproOfficial
quantity_destroyed2 units×1@icpbtrubicon
subtype_descriptionDeep Strike UAV×1@third_svitova
visual_featureforward wings (canards)×1@texBPLA

×N – how many different sources (channels, sites or documents) give this value; ×1 means one.

Components and technologies

ValueSourcesWhere
satellite guidance system (GPS)×1@kcpn2014
solid-fuel rocket booster×2@uav_tech, @kcpn2014
CRPA antenna×5@DniproOfficial, @VictoryDrones, @uav_tech +2
Starlink×3@DniproOfficial, @payloadUAV, @mil_hub
ZTK-150×2@warhistoryalconafter, @mil_hub
internal combustion engines (ICE)×2@uav_tech, @kcpn2014
ZTK 150/Z150×1@texBPLA
CRPA antennas×1@kcpn2014
inertial navigation system (INS)×1@kcpn2014

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