火箭助推滑翔机的飞行原理及应用

Flight principle and application of rocket booster glider

基于新工科教育大背景下,以火箭助推滑翔机在空中的受力特征为研究对象,建立起相应阶段的力学模型基础,进一步得到相应模型方程,然后根据相应物理力学模型,设计制作火箭助推滑翔机模型。这个过程有助于培养学生在实际工作中抓问题主要矛盾的能力和理论结合实际的能力,为新工科背景下的力学教育改革提供借鉴及参考。

Based on the background of new engineering education, the characteristics of the rocket-assisted glider in the air are studied. Through the physical and mechanical analysis, the mechanical model of the corresponding stage were established. The corresponding model equations were obtained, which are used to guide the subsequent model design. Then the rocket booster glider model according to corresponding physical mechanics model is designed and manufactured. It is very important to cultivate students’ ability to grasp the main contradictions in the actual work. It is very important for the effect to provide reference and reference for the reform of mechanics education under the background of new engineering.