Systems › FP-5 "Flamingo"
FP-5 "Flamingo"
In the sources: FP-5 «Фламинго»
Cruise missiles · Fire Point. Facts from open sources (OSINT), each linked to its post or document; translated from Russian by a language model.
Class and role
| Parameter | Value | Sources | Where |
|---|---|---|---|
| Class | Armament | ×2 | @RuporOfBattle, catalogue |
| Subclass | Cruise missiles | ×2 | @RuporOfBattle, catalogue |
| Function | Attack (engagement) | ×2 | @RuporOfBattle, armyrecognition.com |
| Role | Strike | ×2 | @RuporOfBattle, armyrecognition.com |
| Environment | Air — high altitude (>1000 m) | ×2 | isrs.ngo, armyrecognition.com |
| Environment | Air — low altitude (up to 1000 m) | ×2 | isrs.ngo, armyrecognition.com |
Manufacturer and country
| Value | Sources | Where |
|---|---|---|
| Fire Point | ×9 | @RuporOfBattle, catalogue, @ShrikeNews +6 |
| LLC "LDARZ" | ×1 | @warhistoryalconafter |
| LLC "SKB OVT" | ×1 | @warhistoryalconafter |
| LLC "NEFTEMASH" | ×1 | @warhistoryalconafter |
| OJSC "RIVNEAZOT" | ×1 | @warhistoryalconafter |
| Antonov (SE "Antonov") | ×1 | @new_militarycolumnist |
| Milanion Group | ×1 | @oboronka_channel |
Specifications
| Parameter | Value | Sources | Where |
|---|---|---|---|
| Range | up to 3000 km | ×4 | @texBPLA, @battle_technic, @third_svitova +1 |
| Speed | about 500 km/h ≠ sources disagree | ×4 | @voron_fpv, @texBPLA, @oko_gora +1 |
| Flight altitude | less than 50 m | ×4 | @oko_gora, @wargonzo, @voron_fpv +1 |
| Payload / warhead | about 1150 kg | ×3 | @texBPLA, catalogue, @battle_technic |
| Speed | up to 950 km/h | ×2 | @texBPLA, @third_svitova |
| Flight altitude | below 100 feet (below 30 meters) m | ×2 | @DniproOfficial, @yigal_levin |
| Engine | AI-25 (one of the five power plants used) | ×2 | @battle_technic, catalogue |
| classification | heavy strategic cruise missile | ×2 | @RussianArms, @VictoryDrones |
| flight_altitude | low flight altitude to bypass radar posts | ×2 | @RussianArms, @warhistoryalconafter |
| Range | 930+ km from the state border (target hit) | ×1 | @oko_gora |
| Range | long range | ×1 | @my_el_lab |
| Range | long-range | ×1 | @milinua |
| Range | 1250 km | ×1 | @oko_gora |
| Speed | 0.4–0.5M (about 490–610 km/h) on the cruise segment of the trajectory M / km/h | ×1 | @RussianArms |
| Speed | 940 km/h ≠ sources disagree | ×1 | catalogue |
| Speed | 900 km/h ≠ sources disagree | ×1 | catalogue |
| Gross weight | 6000 kg | ×1 | catalogue |
| Payload / warhead | up to 1200 kg | ×1 | @third_svitova |
| Payload / warhead | 1000 kg | ×1 | catalogue |
| Dimensions | imposing dimensions (heavy strategic cruise missile) | ×1 | @RussianArms |
| Dimensions length | 10 m | ×1 | catalogue |
| Dimensions wingspan | 6 m | ×1 | catalogue |
| Dimensions | about 8 meters (length) m | ×1 | @third_svitova |
| Cost | 500000–1000000 USD | ×1 | catalogue |
| accuracy | 14 m | ×1 | catalogue |
| basing | ground-based | ×1 | @warhistoryalconafter |
| category | ground-launched cruise missile | ×1 | @my_el_lab |
| description | turbojet-powered ground-launched cruise missile | ×1 | @warhistoryalconafter |
| engine_count | 5 | ×1 | @texBPLA |
| engine_development | Fire Point is developing its own engine | ×1 | @milinfolive |
| engine_flexibility | designed to be flexible, able to work with different engine types | ×1 | @ShrikeNews |
| engine_original | AI-25 (stocks exhausted, current power plant unknown) | ×1 | @oboronka_channel |
| engine_type | turbojet engine | ×1 | @zhivoff |
| engine_types | the AI-25TL was the first of five engine types the missile was adapted to | ×1 | @payloadUAV |
| engine_types_count | 5 types of jet engines | ×1 | @milinfolive |
| engine_variants | 5 different engine types, including the AI-25TL | ×1 | @ShrikeNews |
| engines_count | 5 different engines over the entire period | ×1 | @third_svitova |
| first_engine | AI-25TL | ×1 | @third_svitova |
| flight_altitude | very low altitude above ground | ×1 | @milinfolive |
| interception_altitude | 8–13 km | ×1 | @RussianArms |
| interception_distance | 25–35 km | ×1 | @RussianArms |
| ir_signature | high; insufficient shielding of the engine nozzle, high exhaust gas temperature | ×1 | @RussianArms |
| launch_location | territory of Sumy Oblast | ×1 | @wargonzo |
| mass_scale_salvo | 6 missiles in one salvo | ×1 | @milinfolive |
| output | hundreds of Flamingos per month (claimed) | ×1 | @RuporOfBattle |
| propulsion | jet engine (turbojet) | ×1 | @RussianArms |
| propulsion | jet engine (cruise missile) | ×1 | @milinfolive |
| propulsion | turbojet engine | ×1 | @warhistoryalconafter |
| range_class | long range | ×1 | @new_militarycolumnist |
| rate_of_fire maximum | 7 missiles per day — maximum capacity missiles/day | ×1 | @payloadUAV |
| rate_of_fire | rather than the achieved rate | ×1 | @payloadUAV |
| speed_claimed_cruise | 700–800 km/h | ×1 | @oko_gora |
| target | strategic facility in Tula Oblast | ×1 | @wargonzo |
| EO converter | higher than that of the AGM-188A Rusty Dagger | ×1 | @RussianArms |
| classification | strategic cruise missile | ×1 | @RussianArms |
| quantity_launched | 10 units | ×1 | @rybar |
| quantity_shot_down | 9 units | ×1 | @rybar |
×N – how many different sources (channels, sites or documents) give this value; ×1 means one.
Design and propulsion
| Parameter | Value | Sources | Where |
|---|---|---|---|
| Power plant | Turbofan (TRDD) | ×1 | catalogue |
| Propulsor | Jet thrust | ×1 | catalogue |
| Motor Sich AI-25 | ×1 | catalogue |
Autonomy and connectivity
| Parameter | Value | Sources | Where |
|---|---|---|---|
| Navigation | Inertial (INS) | ×2 | isrs.ngo, armyrecognition.com |
| Navigation | Satellite (GNSS) | ×2 | isrs.ngo, armyrecognition.com |
| Navigation | Terrain-matching | ×1 | armyrecognition.com |
Components and technologies
| Value | Sources | Where |
|---|---|---|
| turbojet engine | ×3 | @ShrikeNews, @payloadUAV, @third_svitova |
| solid-fuel booster | ×1 | catalogue |
| solid-fuel rocket booster | ×1 | @RussianArms |
| AI-25TL | ×3 | @ShrikeNews, @payloadUAV, @third_svitova |
| AI-25 | ×2 | @texBPLA, @oboronka_channel |
| Motor Sich AI-25 | ×1 | catalogue |
| Composite fuselage | ×1 | catalogue |
| Warhead 1 150 kg | ×1 | catalogue |
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