Research on the Material of the Propellant and Structure Characteristic of the Engine in Miniature

Yao Yao Li; Chun Lan Jiang

doi:10.4028/www.scientific.net/AMM.333-335.1880

Paper Titles

Preparation and Properties of Cage-Like Nano ZnO
p.1862

Effects of Freeze-Thaw Circumstance on Stress and Displacement Filed of Tunnel Surrounding Rock
p.1867

Rheological and Electrical Properties of CB/HDPE Composites
p.1872

The Research on Comparison and Conversion of Two Friction Materials Testing Standards
p.1876

Research on the Material of the Propellant and Structure Characteristic of the Engine in Miniature
p.1880

Research on the Heating Value Measurement of Ethanol-Biodiesel-Diesel Blend
p.1884

Study on Basic Properties and High-Temperature Performance of Rice-Husk-Ash-Modified-Asphalt
p.1889

Quantum Dot Array LED Research with ZnO as an Electron Transport Layer
p.1895

A Novel System for Sedimentary Organic Carbon Isotope Sample Preparation
p.1899

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 333-335Research on the Material of the Propellant and...

Research on the Material of the Propellant and Structure Characteristic of the Engine in Miniature

Abstract:

In order to solve the time of the propellant of the engine in miniature too short, the power of the propellant of the engine is not enough. In this article, the material characteristic of the engine material and the structure characteristic of the engine are analyzed. Also the reliability of the material and the structure characteristic is researched. This article could be used as reference for the design of the rocket engine.

You might also be interested in these eBooks

Measurement Technology and Engineering Researches in Industry

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 333-335)

Pages:

1880-1883

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.333-335.1880

Citation:

Cite this paper

Online since:

July 2013

Authors:

Yao Yao Li*, Chun Lan Jiang

Keywords:

Engine in Miniature, Material in Engine, Mechanism, Reliability, Simulation

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[1] A M Law, W D Kelton. Simulation Modeling and Analysis. 3rd. Ed [M]. (2003).

Google Scholar

[2] GaronKD, Faminu O. Aeroballistic range tests of missle configurations with non-circular cross-sections and aeroprediction comparison results [R]. AIAA 2003. 1243.

DOI: 10.2514/6.2003-1243

Google Scholar

[3] WANG Shan, HE Jian. Missile structure Reliability [M]. Harbin: Harbin Engineering University Press, 2002; 236-243.

Google Scholar

[4] LIU Ying-wei, HOU Jun-ping, Reliability analysis for the deploying mechanism of missile wing [J], Hong du Science and Technology, 2001(1): 1-5.

Google Scholar

[5] NI Jian, LU Kai, ZHANG Duo. Movement function reliability of mechanism of deployable folded wings of missile [J]. Aerospace Shanghai, 2001(5): 1-5.

Google Scholar