Payload carry and launch system

An aerospacecraft comprising:

• a) a fuselage, a pair of wings with a plurality of control surface and a tail with a rudder;
• b) the fuselage comprising:
• i) a conic curve shape for an upper fuselage from a nose end to a tail end;
• ii) a straight line conic shape for a lower fuselage from the nose end to an engine nacelle;
• the engine nacelle aft of a plurality of inlets having a constant semicircular cross section to a plurality of engine exhaust nozzles;
• and a lower aft fuselage having a decreasing concave conic shape to the tail end;
• iii) a maximum cross section dimension of the fuselage is at the wing root leading edge and is such to enclose a payload bay;
• and access to the payload bay is by means of two clam shell doors from the nose end aft being a payload bay hood and a payload bay ramp which may be opened to receive a payload, closed for flight operations and opened for payload removal;
• c) the wings comprising:
• i) a pair of wing strakes added to the fuselage at a centerline to accommodate the wings;
• and
• ii) each wing leading edge is swept back from a strake junction with each wing outer portion curved back to a wing tip;
• d) the tail comprising:
• i) the tail mounted slightly forward of the tail end and a tail leading edge swept back from a tail root;
• and
• ii) a tail outer portion curved back to a tail tip;
• e) an attitude control system with a plurality of attitude control rockets mounted in the payload bay hood and the wing tips with supporting a plurality of position fuel tanks;
• f) a nose gear and a set of mid section landing gears;
• g) an integral ascent tank contained in the fuselage aft of the payload pay, a plurality of auxiliary ascent tanks, and a cradle tank;
• h) an air liquification unit which receives air from the air liquification inlets connected by ducting contained in the engine nacelle and which liquifies the air for storage in a plurality of liquid air tanks;
• i) an avionics system, a plurality of helium tanks and a plurality of primary power propellant units;
• and
• j) a plurality of ejector ramjet engines mounted in the engine nacelle which receive ambient air from the engine nacelle inlets connected by engine inlet ducts.