The influence of the type and size of the reactor and the influence of the heating interruption during curing on the solid composite propellant properties

2021 ◽  
pp. 51609
Author(s):  
Bruno Cesar Christo Da Cunha ◽  
Jose Atilio Fritz Fidel Rocco
Keyword(s):  
Composite Propellant ◽  
Solid Composite Propellant

Recent progress in evaluating the detonation characteristics of solid-composite propellant.

AIAA Journal ◽  
1968 ◽  
Vol 6 (3) ◽  
pp. 489-496
Author(s):  
R. B. ELWELL ◽  
O. R. IRWIN ◽  
P. K. SALZMAN ◽  
N. H. VALOR
Keyword(s):  
Recent Progress ◽  
Composite Propellant ◽  
Solid Composite Propellant ◽  
Detonation Characteristics

Energy Partition in an Impacted or Shocked Solid Composite Propellant

1982 ◽  
Vol 27 (5-6) ◽  
pp. 241-246
Author(s):  
W. H. ANDERSEN ◽  
L F. POLAK ◽  
G. P. STILLMAN
Keyword(s):  
Energy Partition ◽  
Composite Propellant ◽  
Solid Composite Propellant

A nonlinear viscoelastic constitutive model for cyclically loaded solid composite propellant

2020 ◽  
Vol 198 ◽  
pp. 126-135
Author(s):  
Xin Tong ◽  
Jinsheng Xu ◽  
Issam Doghri ◽  
Marieme Imene El Ghezal ◽  
Anouar Krairi ◽  
...  
Keyword(s):  
Constitutive Model ◽  
Composite Propellant ◽  
Nonlinear Viscoelastic ◽  
Solid Composite Propellant ◽  
Viscoelastic Constitutive Model

scholarly journals The use of image analysis for the study of interfacial bonding in solid composite propellant

2007 ◽  
Vol 72 (10) ◽  
pp. 1023-1030 ◽  
Author(s):  
Jasmina Dostanic ◽  
Gordana Uscumlic ◽  
Tatjana Volkov-Husovic ◽  
Radmila Jancic-Heinemann ◽  
Dusan Mijin
Keyword(s):  
Mechanical Properties ◽  
Image Analysis ◽  
Great Influence ◽  
Digital Camera ◽  
Interfacial Bonding ◽  
Composite Propellant ◽  
Bonding Agents ◽  
Solid Composite Propellant

In the framework of this research, the program Image Pro Plus was applied for determining the polymer-oxidizer interactions in HTPB-based composite propellants. In order to improve the interactions, different bonding agents were used, and their efficiency was analyzed. The determination of the quantity, area and radius of non-bonded oxidizer crystals is presented. The position of formed cracks in the specimen and their area have a great influence on the mechanical properties of composite propellant. The preparation of the composite propellant in order to enable the photographing of their structure by means of stereoscopic and metallographic microscopes with the digital camera is also described as well. .

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