载人航天器

未来30年内，美国有可能会把载人航天器送上火星。

In thirty years from now the United States should have a manned spacecraft on Mars .

它还可以坚持像检查商用飞机一样彻底检查私人载人航天器。

It could also insist on checking private manned spacecraft as thoroughly as it does commercial aircraft .

目的设计一种能满足长期载人航天器内固态胺吸附/水蒸气解吸CO2控制系统要求的反应罐。

Objective To design a reaction canister using in solid amine carbon dioxide removal system for long duration spaceflight .

载人航天器SPE水电解制氧系统的轻量化研究

Mass optimization of SPE oxygen generation system in manned spacecraft

太阳耀斑会威胁到环绕地球的所有人造物体，包括全球定位系统（GPS）、通信卫星、载人航天器和国际空间站等。

Solar flares threaten all of the artificial objects orbiting our planet , including GPS and telecommunications satellites , occupied spacecraft and the International Space Station .

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 .

载人航天器或潜艇等密闭环境中CO2的去除和O2及时补充，是环控生保系统的重要任务之一。

Control of CO_2 and O_2 levels within certain range is one of the most important tasks in life support systems , such as spaceship and submarine .

目的解决固态胺CO2吸附方案应用到长期载人航天器座舱中所存在的CO2浓缩与回收问题。

Objective To solve the problem of CO 2 concentration and collection in solid amine CO 2 control system for long duration spacecraft cabin .

为了对载人航天器中SPE制氧系统进行优化改进，根据热力学守恒定律、能量输运规律以及相关电化学理论，建立了系统工作过程的数学模型，通过数值模拟方法对系统进行了性能分析。

A mathematical model including thermodynamics , energy transport and electrochemistry was used to optimize the SPE oxygen generation system in a manned spacecraft .

KM6载人航天器空间环境试验设备

Space Environment Test Facility for Manned Spacecraft

由于载人航天器这一密闭狭小空间及其微重力这一特殊环境，舱内通风空调问题和热舒适环境与地面的HVAC问题不同，微重力效应特别是自然对流大为减弱影响着通风换热效果。

Ventilation , air conditioning and thermal comfort environment of manned spacecraft 's cabin is different to normal HVAC design due to its enclosed and limited space at microgravity . Microgravity effects especially weaken of natural convection affect the ventilation heat exchange .

美国载人航天器的发展史实

History of Manned Space Vehicle in the United States of America

载人航天器的再入制导控制与仿真计算

Guidance , control and Simulation of manned spacecraft in reentry phase

载人航天器并联热网络系统的优化分析

Optimization of the thermal network in parallel connection of manned spacecraft

载人航天器系统人机功能分配方法的研究

Research on Man - Machine Function Allocation of Manned Spacecraft System

载人航天器舱内通风空调特性和数值模拟

Numerical Simulation and Characteristic of Manned Spacecraft Ventilation and Air Conditioning

人在虚拟载人航天器虚拟乘员舱内环境中作业特性的仿真研究

Study on Human Features in Virtual Module Environment of Manned Spacecraft

载人航天器乘员舱结构布局工效学的研究进展。

Ergonomic research on crew module layout in manned spacecraft system .

国外载人航天器回收着陆技术的进展

An Overview of Recovery and Landing Systems for Foreign Manned Spacecrafts

基于遗传算法的载人航天器标准返回轨道设计

Design standard return trajectory of manned spacecraft based on genetic algorithm

应用于载人航天器舱内散热的热管技术研究

Investigation on Heat Pipe Technology for Heat Transport in Manned Spacecraft Cabin

载人航天器电动兼手动舱门的研究

Study on an Electric / Manual Hatch for the Manned Space Vehicles

载人航天器安全性概率算法

A probabilistic approach to safety of the manned space flyer

载人航天器真空热试验技术探讨

The discussion about thermal test techniques in vacuum environment of manned spacecraft

长期载人航天器内务管理信息系统设计

Design of Long Duration Manned Spacecraft Housekeeping Management Information System

载人航天器人&机系统虚拟仿真技术关键问题的探讨

A Study on Key Technology of Man-Machine System Simulation for Manned Spacecraft

载人航天器微量污染净化装置温度控制研究

Study on Temperature Control of Trace Contaminant Control Subassembly in Manned Spacecraft

热钢化对载人航天器舷窗玻璃强度的影响

Effects of thermal tempering on strength of window glass of manned spacecraft

一种载人航天器高压供电系统接地方法

A Grounding Architecture for High-voltage Power System of Manned Spacecraft

载人航天器的发射窗口及太阳能帆板的最佳受晒

Manned spacecraft launching window and solar array optimum sunshine