返回式卫星

阐述了箭上各系统的组成、功能和性能；并以发射返回式卫星和搭载瑞典卫星为例，较详细地给出了CZ-2C的总体性能和飞行程序参数；

The paper introduces the evolution of CZ 2C , the subsystems their schemes , functions and performance , and provides a group of parameters in detail about the overall performance and flight program launching a recoverable satellite and a Sweden piggyback satellite as an example .

选择4株经体外实验筛选出生物学性状变异明显的第20颗返回式卫星搭载的空间培养B16细胞，检测其体内增殖能力及免疫原性的变化。

Four B16 cells , which were on board in the 20th recoverable satellite , are selected . Their biological characteristics are found changed significantly in experiments in vitro .

FSW0型卫星是我国研制的第一种返回式卫星，以其卫星平台为基础又相继发展了FSW1和FSW2型返回式卫星。

FSW - 0 satellite is the first type of recoverable satellites of China . Based on its satellite platform , FSW-1 and FSW-2 were developed in succession .

选择经第20颗返回式卫星搭载的B16细胞，进行体外和体内实验后，筛选出性状变异明显的空间诱变B16细胞株，检测空间诱变B16细胞基因和蛋白质表达的变化。

Four B16 cells which were on board of China 's 20th recoverable satellite were selected whose biological characteristics had changed obviously in the experiments in vitro , in order to detect changes of cells ' expression of proteins and genes .

方法将B16细胞搭载于第20颗返回式卫星，返地后回收细胞，单克隆化，获得110株太空B16细胞，按顺序编号。

Methods B16 cells were carried to the space ( in orbit for 8 days , circle the earth 286 times ) by the 20th Chinese recoverable satellite , and then harvested and monocloned . 110 strains of space B16 cells were obtained in total .

利用所选条件，将细胞搭载于第20颗返回式卫星，空间飞行18d，细胞返回后，经单克隆化，获得110株单克隆细胞，存活率为11%。

B16 cells were carried in the 20th recoverable satellite orbiting 18 days under the optimum conditions . After recovering , 110 strain monocloned cells were survived and the surviving percentage was 1 1 % .

返回式卫星烧蚀防热结构的工程计算

An engineering computation of ablative thermal protection structure of RETURNABLE SATELLITE

我国返回式卫星发展前景及关键技术问题

Prospect and key technology of recoverable satellites in our country

返回式卫星搭载肿瘤细胞和生物工程细胞的初步研究

Preliminary study of tumor cells and bio-engineering cells carried by returned satellite

我国的一种返回式卫星发射时未设整流罩，星体直接受到气动加热。

This paper discusses the problem of aerodynamics heat of non-fairinged satellite .

返回式卫星数字姿态控制系统及飞行试验结果

Digital attitude control system and flight test results of Chinese RETURNABLE SATELLITE

1990年中国返回式卫星的微重力水平监测

Measurement of the microgravity levels in 1990 Chinese RETURNABLE SATELLITE

高粱种子搭载返回式卫星的诱变研究

Study on Induced Mutation of Sorghum Seeds on Recoverable Satellites

多种微生物搭载返回式卫星的试验研究

Experimental Studies of Species of Microorganisms on Board Retrievable Satellite

返回式卫星烧蚀热防护机理与数值模拟

Ablative thermal protective mechanism and numerical simulation for returnable satellite

返回式卫星主动段热控设计

Thermal control design of returnable satellite in launching phase

返回式卫星上的微重力水平估算

Estimation of level of microgravity for recoverable artificial satellite

中国返回式卫星遥感和科学试验

Remote Sensing and Scientific Test On Chinese Recovery Satellite

返回式卫星的供配电系统

Electrical power system of RETURNABLE SATELLITE the power supply and distribution in carbon plants

返回式卫星有源搭载微生物试验结果的初报

Preliminary Report of Microbial Experiments with Space - Microbial - Cultivator on Recoverable Satellite

返回式卫星回收系统的控制问题

Control of recovery system of RETURNABLE SATELLITE

FG-23A返回式卫星制动发动机

FG 23A Retrorocket Motor for Recoverable Satellite

中国成功回收第13颗返回式卫星

China Successfully recovered the 13th recoverable Satellite

利用返回式卫星搭载作物种子并研究其变异机理，进而培育新品种，这已成为一种新型的育种方法。

It is a new breeding method to bring seeds to space by recoverable satellite .

为进行空间生命科学探索研究，研制成功用于返回式卫星搭载的小型生物舱。

A small biocabin was developed for space life sciences research on board the recoverable satellite .

利用返回式卫星开展微重力试验

Microgravity experiment by using recoverable satellite

返回式卫星的最新发展

Recent developments of recovery satellites

根据我国返回式卫星的特点，描述了热惯性法在热设计中的应用。

According to the characteristics of the satellite , a method of thermal inertia used in thermal design is described .

生物卫星设计用于运送和搭载人、动物或其他生物的、人造可返回式卫星。

An artificial , recoverable satellite that is designed to carry and support humans , animals , or other living organisms .

1987年9月第一次被成功地应用于返回式卫星上，以后又多次参加卫星飞行试验，均获得圆满成功。

It was used successfully in the recoverable satellite first in September 1987 and had been used many times since then .