Liquid dispensing lighter-than-air airship system

A hybrid airship, platform system, for delivering and dispensing large quantities of liquid while in flight and hovering modes over specified ground areas, where lift for said airship system is achieved in part by helium confined therewithin, said hybrid airship platform system comprising:

• a.) a semi-rigid, light-weight frame encased within a skin and aerodynamically configured to provide lift in an air stream while in flying and hovering modes over said specified ground areas;
• b.) means for flying said airship system, where said means include a plurality of engine fans and attitude stabilizing mechanisms to provide 3-axis stability and control;
• and
• c.) a liquid control and dispensing mechanism disposed primarily within said frame, said mechanism including,
• i.) a liquid holding tank positioned along the center of gravity of said airship system,
• ii.) a manifold in liquid communication with said holding tank, where said manifold includes means for controlling the quantity of liquid passing therethrough, and
• iii.) a liquid distribution, piping nozzle assembly in liquid communication with said manifold, where said assembly is exposed below said frame;
• wherein said liquid control dispensing means further includes a reservoir, open to the exterior of said airship system, for receiving in-fight replenishing of liquid, to feed liquid to said holding tank.