U.S. double-base solid propellant tactical rockets of the 1940-1955 era

1973 ◽  
Author(s):  
F. WARREN ◽  
C. HERTY, III
Keyword(s):  
Solid Propellant ◽  
Double Base

scholarly journals Study on Main curvature of Stress Relaxation Modulus of a Double-base solid propellant

2021 ◽  
Vol 1965 (1) ◽  
pp. 012023
Author(s):  
Zhang Jian-bin ◽  
Guo Lei ◽  
Li Guang-hua ◽  
Lu Bing-ju ◽  
Cheng Dong
Keyword(s):  
Stress Relaxation ◽  
Solid Propellant ◽  
Relaxation Modulus ◽  
Double Base

scholarly journals Fundamental Burning Characteristics of Double-Base Solid Propellant.

1992 ◽  
Vol 18 (6) ◽  
pp. 881-886
Author(s):  
Seiichi Deguchi ◽  
Hitoki Matsuda ◽  
Masanobu Hasatani ◽  
Kazushige Kato ◽  
Iwao Komai
Keyword(s):  
Solid Propellant ◽  
Double Base

LASER IGNITION CHARACTERIZATION OF N-5 DOUBLE-BASE SOLID PROPELLANT

2002 ◽  
Vol 5 (1-6) ◽  
pp. 284-295 ◽  
Author(s):  
Grant A. Risha ◽  
Kenneth K. Kuo ◽  
Donald E. Koch ◽  
James R. Harvel
Keyword(s):  
Solid Propellant ◽  
Laser Ignition ◽  
Double Base

An elasto-viscoplastic analysis of direct extrusion of a double base solid propellant

2010 ◽  
Vol 41 (9) ◽  
pp. 1110-1114 ◽  
Author(s):  
Baris Kalaycioglu ◽  
M. Husnu Dirikolu ◽  
Veli Çelik
Keyword(s):  
Solid Propellant ◽  
Direct Extrusion ◽  
Double Base

A Study of Experimental Method for Mechanical Properties of Solid Propellant under Hydrostatic Compressive Loading

2013 ◽  
Vol 300-301 ◽  
pp. 789-793
Author(s):  
Jian Bin Zhang ◽  
Yu Tao Ju ◽  
Chang Sheng Zhou
Keyword(s):  
Mechanical Properties ◽  
Solid Propellant ◽  
Compressive Loading ◽  
Engineering Application ◽  
Structural Features ◽  
Operating Principle ◽  
Test Results ◽  
Axial Loads ◽  
Hydrostatic Loading ◽  
Double Base

Mechanical behavior of solid propellant material under multi-axial loads has attracted much attention in engineering application. According to the properties of solid propellant material, a kind of triaxial compressive device for solid propellant material was designed by utilizing the operating principle of the soil triaxial compressive device. The structural features and operating principle were expounded, and some notes should be paid attention during tests, and mechanical properties of a kind of double-base propellant material under hydrostatic loading were investigated, and some very meaningful data and conclusions were obtained. The results show that the yield strength and compressive strength of double-base propellant material under hydrostatic loading have obtained more remarkable enhancement than those without the hydrostatic pressure effect. The experimental device and the test results may lay the foundation for further research into a viscoelastic-plastic constitutive model of solid propellant material.

Solid propellants burning enhancement using foil embedding method

2008 ◽  
Vol 112 (1138) ◽  
pp. 725-732
Author(s):  
H. G. Darabkhanid ◽  
N. S. Mehdizadeh
Keyword(s):  
Burning Rate ◽  
Solid Propellant ◽  
Burning Surface ◽  
New Method ◽  
Published Data ◽  
Solid Propellants ◽  
Embedding Method ◽  
Double Base

Abstract The method of metal embedding is widely employed in solid propellant motors with end-burning configuration, thereby significantly improving the burning rate of the propellants. In this study, the cylindrical foil embedding method is applied to double-base solid propellant, as a new method, and the effects of the type and thickness of the foil on the burning surface, as well as the burning rate, are experimentally investigated. It is shown that by using the foil embedding method, the burning characteristics of solid propellants can be improved. Results have been compared to some available data. To the best of the author’s knowledge there are no published data available on this method.

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