弹道式再入

高级弹道式再入系统安全壳喷淋再循环系统

Advance ballistic reentry system ( ABRS ) containment spray recirculation system

飞弹（飞机的导弹）机动弹道式再入飞行器

Flying bomb ( missiles resembling aircraft ) maneuverable ballistic reentry vehicle

弹道式再入航天器的烧蚀防热结构设计

Ablative thermal protection structure design of return module

弹道式再入飞行器以配平攻角状态返回的轨道计算原理及相应的控制要求

The Calculating Principle of Reentry Trajectory and the Corresponding Control Requirements for a Ballistic Reentry Vehicle in Trim Attack Angle

载人飞船返回舱的烧蚀防热介绍弹道式再入航天器烧蚀防热结构设计，文中说明了方案、材料选择、设计和分析计算。

ABLATIVE THERMAL PROTECTION OF CAPSULE TYPE RE-ENTRY VEHICLE This paper introduces ablative thermal protection structure design of a return module of some satellites .

弹道式再入飞行器一般为轴对称旋成体，但其质心可以偏离对称轴。

The shape of ballistic reentry vehicle generally is axial symmetry , but its mass center may be departure from the axis of its symmetry .

弹道式飞行器再入高度惯性控制方案

The Inertial Controlling Scheme to Reentry Altitude of Ballistic Vehicle

弹道式飞行器再入时，常常要求在规定高度上发出开伞信号，过载延时控制方法误差太大，不能满足精度要求。

The opening parachute signal is required to sent on the fixed height when the vehicle reentry . The height controlled error through axis apparent acceleration can not meet the required precision .

本文从计算高温电离空气的传播参数出发，给出了弹道式洲际导弹再入时等离子鞘的功率传输特性，并讨论了再入通讯频段选择等问题。

From calculating propagation parameters of high-temperature ionized air , this paper gives power transmission properties of ballistic intercontinental missile during reentry , and discusses the problem about selecting of reentry communication bands and so forth .