Manned Systems
H2PLASMARAY 6.66 / 900 - 1,000 kg MTOW
'Water will be the coal of the future.' Jules Verne, The Mysterious Island, 1874
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) |
