inhabited satellite

Monte Carlo method in estimating radiation safty for manned spaceflight;

Monte Carlo方法在载人航天辐射安全性评价中的应用

The Space Operational Medicine is an important branch of Space Medico-Engineering,and plays an important role in manned spaceflight mission so as to ensure the astronaut s health and safety.

航天实施医学是航天医学工程学的重要组成部分,在载人航天型号任务中为保障任务的顺利实施发挥着重要作用。

Finally, the applications of the quadrupole mass spectrometer array in the field of manned spaceflight were summarized.

本文描述了阵列质谱仪的工作原理及体积、质量、功耗、一机多用以及与小型气相色谱和热导检测器联用时所具有的冗余设计等特点 ,介绍了小型阵列质谱仪发展过程中形成的 3种结构类型及性能 ,阐述了小型阵列质谱仪在载人航天中的广泛应

The present paper discusses the adjustable ability and design method of a standard spacecraft reentry trajectory.

分析了弹道──升力式载人飞船再入大气层过程中的轨道机动能力，并据此选取标准再入轨道，最后探讨了各种再入误差源对无制导再入落点的影响，这是飞船再入制导的基础。

Measure on medicial care and rescue for the first Chinese astronaut during manned space flight;

对我国首次载人航天航天员医疗保障及救护措施的探讨

With 40 years development and practice of manned space flight in China,it gradually comes into being.

航天医学工程是伴随着我国近40年载人航天的发展,孕育催生的一门新兴学科,具有特色鲜明的学科理论体系和实践技术方法。

Objective To design a new digital temperature sensor with quartz crystal for manned space flight.

目的设计一种适合载人航天高精度温度测量的数字式石英温度传感器。

Thermo-optical sensitivity and thermal control system for manned spaceship optical windows;

载人飞船光学窗口的热光学灵敏度和热控制策略

In the end, one system model framework in manned spaceship fault diagnosis and decision with neural network is given.

针对载人飞船飞行试验过程中故障理论与决策特点和可能应用的需要,介绍了神经网络技术的发展,分析了神经网络用于故障诊断的典型模型的优缺点,并提出在载人飞船故障诊断和决策中应用神经网络技术的一个系统模型框架,该框架对于建立飞船工程指挥辅助决策系统具有参考价值。

in this paper, a design method for the 3-degree standard return trajectory of the manned spaceship is studied.

本文研究载人飞船三自由度标准返回轨道的设计方法。

Dynamic model for the seat-bumper system reducing the manned spacecraft landing impact;

载人飞船座椅着陆缓冲系统的动力学模型

Objective To verify reliability and safety of the crew support facilities on board manned spacecraft.

目的验证载人飞船乘员支持设备的安全性和可靠性。

A scheme is put forward for solving the contamination problem of indoor environment due to the problems of less dust control and inefficient cross-ventilation of manned spacecraft in process of integrated assembly,which a dust collector with adjustable air flow amount is used.

针对载人飞船在总装过程中因灰尘控制不够和舱内空气不能有效流通而造成舱内环境污染的问题,提出了解决方案。