Laminar supersonic transport aircraft

A laminar supersonic transport aircraft having a forward section and a distal end, comprising:

• a major reverse delta wing portion located between said forward section and said distal end of said aircraft;
• a first set of at least two jet engines located on a top surface of said reverse delta wing;
• a second set of at least two jet engines superposed to said first set of at least two jet engines on a bottom surface of said reverse delta wing;
• a stabilizing vertical tail located near said distal end of said aircraft;
• a stabilizing canard surface located near said forward section of said aircraft;
• and
• a laminar flow control device comprising a network of cooling tubes attached to an inside underneath surface of said reverse delta wing portion with a suitable coolant flowing through said cooling tubes.

A laminar supersonic transport aircraft having a forward section and a distal end, comprising:

• a major reverse delta wing portion located between said forward section and said distal end of said aircraft;
• a plurality of jet engines on a top surface of said reverse delta wing portion and a plurality of superposed jet engines on a bottom surface of said reverse delta wing portion;
• a stabilizing vertical tail located near said distal end of said aircraft;
• a stabilizing canard surface located near said forward section of said aircraft;
• and
• a laminar flow control device comprising a network of cooling tubes attached to an inside underneath surface of said reverse delta wing portion with a suitable coolant flowing through said cooling tubes.