The present invention relates to a rocket propellant. The present invention is to solve difficulty of reusing a conventional rocket propellant. The reusable rocket propellant of the present invention comprises a reusable rocket propellant equipped with a landing propellant which counteracts gravity on one side of a rocket in order to safely land the rocket in parallel with the ground surface. According to the present invention, in order to prevent an expensive rocket propellant from being used only once and discarded, and to reuse the same, the reusable rocket propellant makes safely lands compared to an unstable landing erected at right angle to the ground surface. Therefore, probability of reuse of a rocket without damage can be increased.
본 발명은 종래의 로켓 추진체의 재사용의 어려움을 해결하기위한 발명이다.본발명의 재사용 로켓추진체는 로켓을 보다 안전하게 지면과 평행하게 착지하게 하기 위하여 로켓 의 일측에 중력에 반작용을 하는 착지용 추진체를 장착한 재사용이 가능한 로켓 추진체를 포함하여 이루어 지며 본발명의 재사용 로켓추진체는 엄청난 비용을 들여 만든 로켓 추진체를 한번만 사용하고 폐기하거나 재사용하기 위하여 지면과 직각으로 세워서 불안정하게 착지하는 과정을 보다 안전하게 착지하여 파손없이 로켓의 재사용 확율을 높일수있다.
Reuse rocket
로켓 추진체
2022-08-25
Patent
Electronic Resource
Korean
DEBRIS REMOVAL METHOD, ROCKET RECOVERY METHOD, RECOVERY TYPE ROCKET, ROCKET REUSE SYSTEM, AND ROCKET
European Patent Office | 2025
|Recovery and Reuse of Rocket Propellants
British Library Conference Proceedings | 1997
|Partial Rocket Reuse Using Mid-Air Recovery
British Library Conference Proceedings | 2008
|Recovery and Reuse of a Rocket Launcher
NTIS | 1990
|Partial Rocket Reuse Using Mid-Air Recovery
AIAA | 2008
|