返回舱

下午12时43分，神舟12号在距离地面400公里处进行了首次姿态调整。半小时后，神舟12号返回舱与推进舱分离。

At 12:43 p.m. , Shenzhou-12 performed its first attitude adjustment while 400 kilometers above earth . Half an hour later , its re-entry module separated from the propelling module .

飞船返回舱再入阶段高超声速六分量测力试验研究

Experiment study of hypersonic six-component force measurement for re-entry module in shock tunnel

神舟3号返回舱内的LET分布及吸收剂量

Let distribution and absorbed dose in sz-3 recoverer

周二，中国新型长征五号B大型运载火箭进行首次太空实验，并将这艘柔性充气式货物返回舱发射升空。

The flexible and inflatable capsule was launched on Tuesday aboard the country 's new large carrier rocket Long March-5B for its first test in space .

根据统计能量分析（SEA）法，对某卫星声振环境和某返回舱噪声环境进行了计算分析。

In this paper , vibro-acoustic environment analysis of a certain satellite and environment noise calculation for a kind of reenter cabin are given based on SEA theory .

讨论了载人航天器低空应急救生时返回舱与逃逸飞行器分离时刻Ta的计算方法。

An algorithm for separation time T a of manned spacecraft reentry capsule from escape system is discussed .

LS-DYNA的ALE方法在飞船返回舱着落仿真中的应用

Simulations of the landing of manned spacecraft with parachutes using the ALE method in LS-DYNA

然后提出了基于近似解的返回舱与逃逸飞行器分离时刻Ta的实时确定方法；

Then , a real-time algorithm for separation time T a is presented , which is based on the approximate solution .

方法：通过HybridIII型假人，在航天返回舱座椅环境中，进行不同输入量级的复合冲击实验和相关的数据分析。

METHODS : Using Hybrid III dummy to put in the backing cabin of space , experiments on landing impact of all levels were carried out and related data were analyzed .

在返回舱的应用中，将SEA法预示结果与曲线拟合方法预示结果及试验结果相比较，结果说明三者一致。

In the reenter-cabin application , the predicted environment results of SEA are compared with results of curvefitting method and test . It shows from the comparation chart that the predicted results is consistent with the results using curvefitting method and acoustic test .

通过数值求解NS方程，进行了三方面工作：（1）格式和算法对返回舱跨声速流场特性的影响研究；

With solving NS equations , the following works have been done : ( 1 ) the study of the effect of scheme and algorithm on transonic flows over blunt body ;

CZ-2F返回舱和逃逸飞行器分离试验技术

The Separation Test Technology of LM-2F ′ s Return Module and Escape Vehicle

方法：3株肿瘤细胞系在专门设计的常温细胞长期生存装置中培养，密封固定于卫星返回舱内，由神州4号运载火箭发射，在太空中飞行7d后回收。

Methods : Three lines of tumor cells were cultured in the special designed outer space cell living system , and was sealed in the returning module of the shuttle , launched by the No. 4 Shenzhou carrying space shuttle , returning in 7 days after flying in outer space .

不带稳定翼飞船返回舱俯仰动稳定性研究

Study of the dynamic stability of a pitching unfinned reentry capsule

本文主要介绍小升阻比载人飞船返回舱的配平气动特性。

This paper introduces the trim aerodynamic characteristics of re-entry modules .

返回舱水上冲击特性的试验研究与理论计算

Tests and calculations of water impact characteristics of a recovery module

返回舱和着陆系统设计的新理念

New Concept of Design for Crew Return Vehicle and Landing System

飞船返回舱再入飞行迎角和侧滑角估计

Angle-of-attack and sideslip-angle estimation of reentry capsules of spacecraft in reentry flight

应急救生时返回舱分离后的姿态运动研究

Attitude Motion of Return Module after Separation in Emergency Surviving

载人飞船返回舱着陆救生辅助决策系统研究

The Study of Landing-rescue Aid-decision System of Return Capsule of Manned Spaceship

飞船返回舱俯仰振荡的动态稳定性研究

Research on the dynamic stability of an orbital reentry vehicle in pitching

该返回舱预计可重复使用10次左右。

The return capsule is expected to be reused around 10 times .

飞船由轨道舱、返回舱和推进舱组成。

The unmanned spacecraft consists of orbit , descent and propulsion modules .

中国神州号载人飞船返回舱防热材料现状及展望

Status & Prospect of thermal protective materials on china 's Shenzhou spacecraft

可控翼伞、返回舱组合体滑翔性能研究

Research of gliding performances for the assembly of Controllable Parafoil and recovery module

返回舱弹道重建与黑障区弹道再现研究

Trajectory reconstruction and black-out - area trajectory makeup for reentry capsules of spacecraft

本文发展了基于弹道重建的返回舱迎角和侧滑角估计方法。

An angle-of-attack and sideslip-angle estimation method is developed based on trajectory reconstruction .

“实践八号”卫星返回舱在四川省遂宁县落地回收。

The satellite 's return capsule was recovered in Suining , Sichuan Province .

飞船返回舱座椅缓冲系统的改进与优化设计

Improvement and optimal design of a seat-buffer system in reentry capsule of spacecraft

内在安全，工厂焊接弹簧返回舱。

Inherently safe , factory welded spring-return module .