strap-on launch vehicle

The research proves that the correlation of modal test/ analysis shows good agreement and the analysis model of dynamic characteristic calculation for heavy lift strap-on launch vehicle.

相关性研究表明，试验/分析结果的相关性相当好，大型捆绑火箭动特性计算的分析模型是精确的。

Analysis on Torsional Vibration and Longitudinal Vibration of Strap-on Launch Vehicle Boost Phase

捆绑型火箭助推段扭转与纵向振动耦合的分析

This paper gives a algorithm ( point by point method) to solve them, and analyzes the modal of strap-on launch vehicle.

本文阐述了用逐点计算法求解捆绑火箭模态的计算模型和计算方法，并对带助推火箭的火箭模态进行了分析。

Lateral Vibration Modal of Strap-on Launch Vehicle

捆绑火箭的横向振动模态

The Natural Vibration Performance Analysis of Lateral Vibration for the Launch Vehicle of Strap-on Boosters

捆绑式运载火箭横向振动的固有特性分析

Attitude control is a key technology for the development of large strap-on launch vehicle.

姿态控制技术是大型捆绑火箭研制中的关键技术之一。

Dynamic Characteristic Research for the Strap-on Launch Vehicle

捆绑式运载火箭动力学特性研究

A Simple Method to Calculate the Strength and Rigidity of the Launching Pad of CZ-ZE Strap-on Launch Vehicle

CZ－2E发射台强度与刚度计算的一种简易方法

Attitude control system of a large-scale Strap-on Launch Vehicle

大型捆绑运载火箭姿态控制系统

Long March 2E, a large strap-on launch vehicle developed by China, represents a major achievement of the country in space launch technology.

长征二号E是中国最新研制出来的一种大型捆绑式运载火箭。

The article describes a simple method to calculate the strength and rigidity of the launching pad of CZ-ZE strap-on launch vehicle newly developed by CALT.

文章阐述了我国最新研制的CZ－2E捆绑式运载火箭发射台强度与刚度计算的一种简便方法。

A general attitude dynamic model of strap-on launch vehicle is established.

2建立了大型捆绑火箭的通用姿态动力学模型。

Aerodynamic computations for launch vehicle with strap-on boosters air breathing engine technology for Aero-Space plane

捆绑式运载火箭气动力计算空天飞机吸气式发动机技术