Hydrogen Powered Vertical Take-Off And Landing Aircraft

A vertical take-off and landing aircraft, said aircraft comprising:

• a main body fuselage;
• a left wing rotatably coupled to said main body fuselage;
• a right wing rotatably coupled to said main body fuselage;
• a plurality of left side propulsion assemblies coupled to said left wing, wherein said plurality of left side propulsion assemblies comprise:
• a left side outboard propulsion assembly;
• a left side inner upper propulsion assembly;
• a left side inner lower propulsion assembly, wherein said left side inner upper propulsion assembly is coupled to a top end of a left side vertical pylon coupled to said left wing, and wherein said left side inner lower propulsion assembly is coupled to a bottom end of said left side vertical pylon, and wherein said left side vertical pylon is coupled to said left wing;
• a plurality of propulsion assemblies coupled to said right wing, wherein said plurality of right side propulsion assemblies comprise:
• a right side outboard propulsion assembly;
• a right side inner upper propulsion assembly;
• a right side inner lower propulsion assembly, wherein said right side inner upper propulsion assembly is coupled to a top end of a right side vertical pylon coupled to said right wing, and wherein said right side inner lower propulsion assembly is coupled to a bottom end of said right side vertical pylon, and wherein said right side vertical pylon is coupled to said right wing;
• a first hydrogen fuel tank in a forward portion of said main body fuselage;
• a second hydrogen fuel tank in a rearward portion of said main body fuselage;
• and
• one or more fuel cells residing in said main body fuselage.