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Manned Systems


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.


 









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)



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