Title:
VERTICAL FLIGHT SYSTEM TO WHICH MAINLY A ROCKET PROPULSION PRINCIPLE (PRESSURE THRUST, ETC.) IS APPLIED, AND REUSE SPACE SHUTTLES OF (COMPRESSED) AIR CIRCULATION TYPE LOCALLY USING (PARTS) OF THE SYSTEM
Document Type and Number:
Japanese Patent JP2017114467
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To provide versatile reuse space shuttles using highly propulsion-efficient vertical taking-off/landing machines and parts of the vertical flight system of a special VTOL machine without needing any special high-performance (high-cost) engine.SOLUTION: Briefly put, vertical taking-off/landing machines are configured to effectively use the flight principle (pressure thrust, etc.) of a rising rocket while countering a certain gravitational force as roughly illustrated in FIG. 2, etc. In particular, water (liquid) larger in reaction mass (favorable for environment) than combustion gas (gas) such as exiting rocket fuel is efficiently and powerfully injected according to the force of compressed air (maximum air of tens of atmospheric pressure).SELECTED DRAWING: Figure 2
Inventors:
KAMIUCHI KINGO
Application Number:
JP2016107994A
Publication Date:
June 29, 2017
Filing Date:
May 30, 2016
Export Citation:
Assignee:
GRACEMARIE WORLD CORP
International Classes:
B64C29/00