1) Rocket ablation mode (RAM)
火箭烧蚀模式
2) Rocket mode
火箭模式
1.
The paper presents the concept of a nano-sat launch system based on laser propulsion with combination of air-breathing mode and rocket mode.
建立了大气吸气模式与火箭模式组合的激光推进运载器(光船)发射微小卫星入轨的系统概念和分析模型,考虑了推进系统性能、大气传输衰减、模式转换高度、激光器功率、大气飞行阻力、发射点高度等因素对发射系统性能的影响,并对光船发射轨迹进行了计算和讨论。
3) Ablation mode
烧蚀模式
1.
Using high power pulse TEA-CO-2 laser and Ktype thermocouple,the temperature distribution on a parabolic reflector and the temperature response under different pulse number and atmospheric pressure were investigated in air-breathing and ablation mode,respectively.
在激光脉冲个数确定的条件下,大气呼吸模式的温度随气压的减小先增大后减小,出现一个峰值;烧蚀模式则随气压的减小而增大。
4) Ablative mode
烧蚀模式
1.
Adopting the numerical method of differential equation to solve the motion equations of micro-aircraft propelled by pulse ground based laser,the flight characteristics of aircraft in air-breathing mode,ablative mode and combining air-breathing mode with ablative mode are discussed.
采用微分方程数值解法计算地基脉冲激光推进轻型飞行器的运动方程,分析了大气呼吸模式、烧蚀模式以及两种模式相结合方式下飞行器的飞行特点。
5) incendiary rocket
燃烧火箭弹
6) Gun ablation wear
火炮烧蚀
补充资料：弹头烧蚀(见弹头防热)
弹头烧蚀(见弹头防热)
warhead ablation
dantou shaoshi弹头烧蚀(warhead的lation)见弹头防热。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条