探空火箭

寻求探空火箭最佳推力策略的一种直接优化方法

A Direct Method to Search out the Best Thrust Plan for Sounding Rocket

探空火箭动力系统优化设计

Design optimization of propulsion system of sounding rocket

根据探空火箭可视化仿真及协同设计系统的目标，进行了需求分析。进而设计了基于HLA的可扩展的系统体系结构。

Based on the needs analysis , scalable system architecture based on HLA was then designed .

在这个体系结构下，利用HLA平台对互操作性和重用性的支持，实现仿真和设计过程的协同，支持不同型号、不同有效载荷多种探空火箭应用项目的仿真、设计和论证。

In this architecture , with support from the interoperability and reusability of HLA platform , synergy of simulation and design process can be achieved .

TY-3探空火箭突起物气动加热计算

Calculation of aerodynamic heating for the protuberances on TY-3 sounding rocket

我国海南探空火箭首批发射试验成功及其科学意义

Scientific significance of launching sounding rockets from Hainan in China

我国第三代探空火箭的发展概况

Development of the third generation sounding rockets of China

一种优选探空火箭总体设计方案的方法

A Method of Optimization of Sounding Rocket Architectural Design

和平号探空火箭轻便式气球、火箭高空大气探测共用系统

A portable sharing upper atmospheric sounding system used by both balloon and micro-rocket

风对探空火箭飞行弹道影响的分析

Analysis of wind effects on sounding rocket trajectory

761探空火箭推进剂的研制

Development for " 761 " Sounding Rocket Propellant

ZN&3探空火箭头罩分离的分析及弹射分离器的设计

The analysis of the separation of ZN-3 sounding rocket nose cap and catapult separator design

761探空火箭喷管绝热内衬的工艺探讨

Study of the Technological Process of Adiabatic Bush for 《 761 》 Sounding Rocket Nozzle

探空火箭是在近地空间进行探测和科学实验的火箭。

Sounding rocket is a kind of rocket for sounding and scientific experiments in Near-Earth Space .

瑞典的探空火箭综述

An Overview of Swedish Sounding Rockets

中国在二十世纪六十年代初期开始利用探空火箭、探空气球开展了高层大气探测。

China started to explore the upper atmosphere using rockets and balloons in the early 1960s .

和平号探空火箭气象条件对远程火箭炮射击精度的影响及对策

Influence and Countermeasure of Meteorology Condition for Shooting Precision of Certain Type of Long-range Rocket Launcher

仅靠一个电话线杆大小的探空火箭就能把一个人送入太空。

You couldget a person to space with a rocket the size of a telephone pole .

提出了探空火箭动力系统设计参数优化计算方法。

An calculating method for design parameter optimization of the propulsion system of the sounding rocket is given .

对于空间研究活动的援助是通过联合国支助的两个探空火箭发射站进行的。

Space research activities are being aided through two sounding rocket launching stations sponsored by the United Nations .

此外，一种新型号探空火箭&织女三号高空研究火箭也将于近年内发射。

A kind of new rocket , vega-3high altitude research rocket , will launched in the near furture .

进一步开展从地面站、探空火箭和气球探测取得更多的地基现场观测数据的工作。

Ground-based in situ observations will be enhanced from ground stations as well as from sounding rockets and balloons .

探空火箭风场补偿及等效弹道风转化

The Wind Compensation of Ballistic Trace of a Low Altitude Sounding Rocket with the Translation Model from Variable Wind to Constant Wind

由无控固体探空火箭和地面发射设备组成的运载系统是固体火箭探空系统的一个组成部分。

The carrier system that consists of an unguided solid sounding rocket and a set of launching facilities is a part of solid rocket sounding system .

叙述了进行地面研究的指导思想，分析了所使用的地面实验设施（落塔，抛物线飞行，探空火箭等）。

The concept of ground based research is introduced and the ground facilities ( i.e. drop towers , parabolic flights , sounding rockets ) used are analysed .

主要用于探空气球和微型火箭对高空大气探测数据的接收和处理。

It is mainly used to receive and process the data from balloons and micro-rockets .

从探空七号气象火箭到织女三号高空研究火箭&我国实用探空火箭发射成功30年回顾

From SOUNDING-7 meteorological rocket to VEGA-3 high altitude research rocket & review the past thirty years since the first successful launch of SOUNDING-7 rocket

高精度大气压力传感器在地面气象站及探空气球与探空火箭中有着广泛的应用，该传感器的精度直接影响了气象预报的准确度。

The high precision barometers have been applied widely in weather station , sounding balloon and sounding rocket , its precision directly works on the accuracy of weather forecast .

介绍了中国实用火箭探空系统的种类、实用探空火箭的性能参数和飞行情况、火箭探空取得的技术进步和存在的问题。

The kinds of the Chinese practical rocket sounding systems , performance parameters and flying condition of the chinese practical sounding rockets , technology progress and present problems of the Chinese rocket sounding in the 20th century are introduced .