Manned Systems
'Water will be the coal of the future.' Jules Verne, The Mysterious Island, 1874
H2PLASMARAY 6.66 / 900 - 1,000 kg MTOW
PLASMARAY 1.11 and H2PLASMARAY 1.11 UAV systems are plasma flow controlled, swarm capable eVTOL demonstrators for a new class of hydrogen fuel-cell powered, hyperfast air taxis with 6.66 m (900 - 1,000 kg), 8.88 m (1,850 - 2,000 kg), 11.1 (3,000 kg), 13.3 m (5,700 kg), 18.0 m (10,500 kg) and 19.9 m (13,500 kg) wingspan. The H2PLASMARAY 18.0 Strato and H2PLASMARAY 19.9 Strato will be futuristic near-space tourism vehicles using our novel magnetoplasma jet propulsion to climb up to very high altitudes of +30 km, but can also be used as long-range heavy cargo lifters without the additional plasma propulsion.
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TECHNICAL SPECIFICATIONS
H2PLASMARAY 6.66 | LH2PLASMARAY 6.66 | |
Passengers / Pilots: | 2 | 2 |
Length: | 4.67 m | 4.67 m |
Wingspan: | 6.66 m | 6.66 m |
Maximum Take-off Weight (MTOW): | 900 kg | 920 kg |
Empty Weight: | 346 kg | 352 kg |
Battery Weight: | 137 kg | 137 kg |
Fuel Cell System Weight: | 167 kg | 181 kg |
Payload / Passenger Weight: | 250 kg | 250 kg |
Cruise Speed: | 250 - 291 km/h (135 - 157 knots) | 250 - 291 km/h (135 - 157 knots) |
Maximum Cruise Speed: | 270 - 314 km/h (146 - 170 knots) | 270 - 314 km/h (146 - 170 knots) |
Flight Range: | 250 km (H2) | 1000 km (LH2) |
Flight Time (with 2 - 3 min VTOL): | 1 hour (H2) | 4 hours (LH2) |
Flight Altitude: | 0 - 3,000m (0 - 10,000 ft) | 0 - 3,000m (0 - 10,000 ft) |
Maximum G-Limit: | +5 | +5 |
Total Energy (Battery + Fuel Cells): | 89 kWh (26 kWh + 63 kWh) | 225 kWh (26 kWh + 199 kWh) |
VTOL Power: | 560 - 669 kW | 560 - 669 kW |
Cruise Power: | 46 kW | 46 kW |
First Flight: | 2023 | 2024 |
Electric Ducted Fan Motor: | 19+19 Schübeler DS-215-DIA HST (195 mm) for eVTOL (38x 27 kg or 1,026 kg, 669 kW) and 10 DS-215-DIA HST for cruise (max. 270 kg for runway take-off) or 9+9 VasyFan VF-390 for eVTOL (18x 60 kg or 1,080 kg, 560 kW) and 8 VasyFan VF-250 for cruise (max. 450 kg for runway take-off with 50% thrust-to-weight ratio) or 7+7 VasyFan VF-390 for eVTOL (14x 75 kg or 1,050 kg, 644 kW) and 8 VasyFan VF-250 for cruise (max. 450 kg for runway take-off with 50% thrust-to-weight ratio) or 4+4 VasyFan VF-570 for eVTOL (8x 150 kg or 1,200 kg) and 8 VasyFan VF-250 for cruise (max. 450 kg for runway take-off with 50% thrust-to-weight ratio) | 19+19 Schübeler DS-215-DIA HST (195 mm) for eVTOL (38x 27 kg or 1,026 kg, 669 kW) and 10 DS-215-DIA HST for cruise (max. 270 kg for runway take-off) or 9+9 VasyFan VF-390 for eVTOL (18x 60 kg or 1,080 kg, 560 kW) and 8 VasyFan VF-250 for cruise (max. 450 kg for runway take-off with 49% thrust-to weight ratio) or 7+7 VasyFan VF-390 for eVTOL (14x 75 kg or 1,050 kg, 644 kW) and 8 VasyFan VF-250 for cruise (max. 450 kg for runway take-off with 49% thrust-to-weight ratio) or 4+4 VasyFan VF-570 for eVTOL (8x 150 kg or 1,200 kg) and 8 VasyFan VF-250 for cruise (max. 450 kg for runway take-off with 50% thrust-to-weight ratio) |
