Next Generation Aircraft

•  Type: Advanced eVTOL (Electric Vertical Take-Off and Landing)
•  Design: Dual-cabin, saucer-top hybrid-lift platform
•  Mission Profiles:

                        o Urban/Regional Cargo Transport

                        o Emergency Response & Surveillance

                        o Executive or Military Liaison Use

                       o ISR or Reconnaissance (with modular payload)

• Lightweight carbon composite   
• Configuration:

                      o Central cargo module suspended from circular propulsion disc      

                      o Telescoping landing struts for uneven terrain 

•  Length (diameter): ~7.5m (25ft)
•  Height: ~3.2m  (10ft) with gear deployed
•  Empty Weight: ~1,400 kg (3,000lbs)
•  Max Takeoff Weight (MTOW): ~2,200 kg (5,000lbs)
•  Cabin Capacity: 2–4 passengers (configurable)

•  Flight System: AI-enhanced fly-by-wire with redundancy
•  Navigation: GNSS, inertial + LIDAR-based terrain mapping
•  Autonomy Level: L4+ (optional manual override via joystick control)
•  Interface: Transparent AR HUD with voice and gesture input
•  Comms: Encrypted mesh networking with 5G/LTE fallback

          •  Lift System:

                    o  8x coaxial ducted fan units (EDF) embedded in saucer disk

                    o  Adaptive pitch & vectored thrust for 6DOF control

          •  Powertrain:

                    o  Dual redundant  battery banks (800V architecture)

                    o  Optional hybrid generator module for extended range

           •  Endurance:

                    o Pure electric: ~300–700 km range (187-434 miles)

                    o Hybrid assist: up to 3500 km   (2100 miles)

           •  Cruise Speed: ~150 km/h (93 mph)

          •  Max Speed: ~220 km/h (137 mph)

          • Cooling:

                   o naturally aspirated battery matrix

                   o Independent avionics and cabin climate loop

          • Solar Option: Thin-film solar cells on disc top 

          •  Emergency Systems:

                     o  Ballistic parachute capsule ejection (auto-deploy)

                     o  Independent flight control backups

          •  Collision Avoidance:

                    o  360° sensor fusion (LIDAR, radar, optical)

                    o  Predictive obstacle tracking

          •  Failover:

                      o  Isolated power bus and rotor group segmentation

          •  Payload Modules:

                   o  ISR sensor bay

                   o  Medical support pod

                   o  Cargo delivery platform

          • Software: OTA firmware updates via secure link

          •  Ground Docking: Automated charging and data sync platform