초록 ▼

The present invention relates to an aircraft having a plurality of fuselages for increased payload. More specifically, the aircraft has a central fuselage, and first and second side-saddle fuselages mounted on opposite sides of the central fuselage. The first and second side-saddle fuselages further

The present invention relates to an aircraft having a plurality of fuselages for increased payload. More specifically, the aircraft has a central fuselage, and first and second side-saddle fuselages mounted on opposite sides of the central fuselage. The first and second side-saddle fuselages further are provided with a mechanism for opening and each of the side-saddle fuselages define a launch tube such that each launch tube is adapted for transporting and launching a large or oversize missile.

대표청구항 ▼

1. An aircraft comprising: A plurality of longitudinally extending fuselages sidewardly joined along a common horizontal plane, said plurality of longitudinally extending fuselages comprising a central fuselage and first and second side-saddle fuselages mounted on opposite sides of said central fuse

1. An aircraft comprising: A plurality of longitudinally extending fuselages sidewardly joined along a common horizontal plane, said plurality of longitudinally extending fuselages comprising a central fuselage and first and second side-saddle fuselages mounted on opposite sides of said central fuselage, said first and second side-saddle fuselages provided with a means for opening and further defining first and second launch tubes wherein each of said first and second launch tubes is adapted for transporting and launching a missile.