CAJ | 학술논문

针对配用涡轮解保引信单兵火箭弹高原和平原条件下解保距离试验，得出不同结果，根据结果，定性分析影响引信解除保险距离性能的关键因素，定量计算高原环境下引信解除保险距离的变化，针对涡轮解保引信此特性，提出从空气动力学角度对引信解除保险距离偏长原因进行理论和仿真分析，通过该方法仿真计算获取在不同海拔高度条件下的引信解除保险距离，建立了引信解除保险距离与空气密度之间的数学模型，为引信在不同条件下使用提供参考。
침대배용와륜해보인신단병화전탄고원화평원조건하해보거리시험，득출불동결과，근거결과，정성분석영향인신해제보험거리성능적관건인소，정량계산고원배경하인신해제보험거리적변화，침대와륜해보인신차특성，제출종공기동역학각도대인신해제보험거리편장원인진행이론화방진분석，통과해방법방진계산획취재불동해발고도조건하적인신해제보험거리，건립료인신해제보험거리여공기밀도지간적수학모형，위인신재불동조건하사용제공삼고。
Individual rocket turbine fuze test in plateau and plain had different results,according to the results, the key influence factors were qualitatively analysed,and the arming distance changing was quantitively calculat-ed.Aerodynamic theoretical analysis and simulation for arming distance were carried out under the different ele-vation height condition of arming distance.the mathematical model of arming distance influenced by air density was established under different condition basis.