{"timestamp_utc": "2026-05-25T06:21:21.587360+00:00", "stage": "stage_2_view_selection", "provider": "anthropic", "model": "claude-haiku-4-5-20251001", "pricing_source": "https://docs.anthropic.com/en/about-claude/pricing", "usage": {"input_tokens": 63509, "output_tokens": 3304, "total_tokens": 66813}, "cost_estimate_usd": {"input_cost_usd": 0.063509, "output_cost_usd": 0.01652, "total_cost_usd": 0.08002899999999999}, "screenshots_sent": 6, "title": "Hybrid VTOL UAV", "description": "Луна (Luna) - echo in Ukrainian\n\nAcknowledgments\nI thank the GrabCAD members whose models I used in this project\nElectronic elements of the control system\nhttps://grabcad.com/riley.entropy-1/models?page=1\nRotoMotor and servo drive\n\nSpeed controller\n\n\nbatteries as a source of energy for lifting electric motors and\nliquid fuel (gasoline) for the cruise ICE\n4 electric motors and at least 2 takeoff-landing cycles, total 0.376 ~ 0.4 kWh\n(with the cruise ICE NOT running)\nMAD 6S 10Ah Drone Solid State Lithium-ion Battery\n\n10000 mAh 222 Wh 152*60*45 mm 0.841kg\n2 batteries = total capacity 0.444 kWh, weight 1.682 kg\nROTO 85 FS UAV ICE\n\nHorizontal flight mode\nCruising speed 25m/s (90km/h)\nRequired thrust ~ 7.5 kG ~ 1.5 kW (< 50%)\nPropeller adjustable (on the ground) pitch 25''/ 4000 RPM\nFuel consumption ~ 0.53 kg/h\nFuel tank – 6 kg fuel (8 liters) = Flight time 11h (1000 km )\nEngine equipped with starter-generator 300/1300 W"}
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