Ekranoplan "Lun" project 903

Modification Lun Wingspan, m 44.00 Length, m 73.80 Height, m 19.20 Wing area, m2 550.00 Weight, kg Empty aircraft 243000 Maximum takeoff 380000 Type 8 turbojet engine NK-87 Thrust, kgf 8 x 13000 Maximum speed, km / h 500 Range, km 2000 Height of the flight on the screen, 1.5 m Seaworthiness, 5.6 points Crew 10 Armament: 6 IP PKR ZM-80 Mosquito


retrodynamic said...

Technology Submission - State of the Art - Novel InFlow Tech - Featured Project Development;|/ ·1; Rotary-Turbo-InFlow Tech / - GEARTURBINE PROJECT Have the similar basic system of the Aeolipilie Heron Steam Turbine device from Alexandria 10-70 AD * With Retrodynamic = DextroRPM VS LevoInFlow + Ying Yang Way Power Type - Non Waste Looses *8X/Y Thermodynamic CYCLE Way Steps. Higher efficient percent. No blade erosion by sand & very low heat target signature Pat:197187IMPI MX Dic1991 Atypical Motor Engine Type /·2; Imploturbocompressor; One Moving Part System Excellence Design - The InFlow Interaction comes from Macro-Flow and goes to Micro-Flow by Implossion - Only One Compression Step; Inflow, Compression and outflow at one simple circular dynamic motion / New Concept. To see a Imploturbocompressor animation, is possible on a simple way, just to check an Hurricane Satellite view, and is the same implo inflow way nature.

Post a Comment