Remote control flying model spaceship

A spaceship comprising:

• a propulsion duct having a tubular form with an inside periphery, an outside periphery, an intake end and a discharge end;
• a ducted fan having a fan shaft concentric to a linear axis of the propulsion duct and positioned inside of the intake end of the propulsion duct;
• a rotational prime mover attached to the propulsion duct and having rotational-drive relationship to the fan shaft;
• a circular wing having a low-dome contour on a central top surface of the circular wing such that laminar flow of air over a leading edge of the circular wing and lift vacuum over an aft portion of the circular wing are induced from forward movement of the circular wing propelled by the ducted fan when the ducted fan is rotated by the rotational prime mover;
• rotatable attachment of a center of the circular wing to a pivotal wing axle on the forward strut;
• a first pod wing having aerodynamic-lift surfaces and attached to a first side strut extended sidewards and upwards at a select angle from a first side of an intermediate portion of the outside periphery of the propulsion duct;
• a second pod wing having aerodynamic-lift surfaces and attached to a second side strut extended sidewards and upwards at a select angle from a second side of an intermediate portion of the outside periphery of the propulsion duct;
• a stabilizer wing extended horizontally between the first pod wing and the second pod wing;
• an aileron attached pivotally to each pod wing;
• an elevator attached pivotally to a rear edge of the stabilizer wing;
• a thrust tube having an inside periphery in laterally-pivotal relationship to the inside periphery of the discharge end of the propulsion duct such that air discharged from the discharge end of the propulsion duct can be directed in either side direction to steer the spaceship without a rudder or vertical stabilizer;
• and
• a remote controller in remote radio-wave-control communication with the aileron attached pivotally to each pod wing, the elevator attached pivotally to a rear edge of the stabilizer wing and the thrust tube.

A spaceship comprising:

• a propulsion duct having a tubular form with an inside periphery, an outside periphery, an intake end and a discharge end;
• a ducted fan having a fan shaft concentric to a linear axis of the propulsion duct and positioned inside of the intake end of the propulsion duct;
• a rotational prime mover attached to the propulsion duct and having rotational-drive relationship to the fan shaft;
• a circular wing attached to a forward strut extended upward vertically and forwardly from a front portion of the outside periphery of the propulsion duct;
• a delta wing section extended laterally from each side of the circular-edged wing;
• an aerodynamic-lift surface on top of the circular-edged wing integrated with an aerodynamic-lift surface on top of each delta wing section such that the circular-edged wing and the delta wing sections form a single wing having a circular leading edge with delta-shaped side portions;
• a first pod wing attached to a first side strut extended sidewards and upwards at a select angle from a first side of an intermediate portion of the outside periphery of the propulsion duct;
• a second pod wing attached to a second side strut extended sidewards and upwards at a select angle from a second side of an intermediate portion of the outside periphery of the propulsion duct;
• a stabilizer wing extended horizontally between the first pod wing and the second pod wing;
• an aileron attached pivotally to each pod wing;
• an elevator attached pivotally to a rear edge of the stabilizer wing;
• and
• a thrust tube having an inside periphery in laterally-pivotal relationship to the inside periphery of the discharge end of the propulsion duct such that air discharged from the discharge end of the propulsion duct can be directed in either side direction to steer the model spaceship without a rudder or vertical stabilizer.