发明名称 METHOD FOR LAUNCHING SPACE ROCKET
摘要 PROBLEM TO BE SOLVED: To solve the following problem: since the speed of a space rocket is slow for a while from when it is started in a conventional launching method, launch has failed many times. SOLUTION: A cannon which is a conventional well-known industrial product as well as a firearm can fly a bullet at a high speed while forming a straight trajectory immediately after the stating time when the bullet is fired and for a little while from that time. Therefore, a structure imitating the mechanism of the cannon is used as the launcher of the space rocket to forcibly launch the space rocket from the launcher, immediately after that, fuel is ignited before the speed reduces, and the space rocket is accelerated to increase kinetic energy. Thereby, even if the space rocket is influenced by external force generated from various natural phenomena, the space rocket can continue its fly without disturbing the straight trajectory, and objective to surely make the space rocket reach a highly vacuum space with no gravity from the ground can be accomplished. COPYRIGHT: (C)2008,JPO&INPIT
申请公布号 JP2008132957(A) 申请公布日期 2008.06.12
申请号 JP20060357092 申请日期 2006.11.27
申请人 KURIBAYASHI MASAFUMI 发明人 KURIBAYASHI MASAFUMI
分类号 B64G5/00 主分类号 B64G5/00
代理机构 代理人
主权项
地址