2018
DOI: 10.1080/07370652.2018.1441925
|View full text |Cite
|
Sign up to set email alerts
|

Study of effect of binders and loading pressures on the performance of the time delay pyrotechnic compositions

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1

Citation Types

0
3
0

Year Published

2020
2020
2024
2024

Publication Types

Select...
7

Relationship

0
7

Authors

Journals

citations
Cited by 10 publications
(3 citation statements)
references
References 9 publications
0
3
0
Order By: Relevance
“…Therefore, they affect sensitivity to friction and ESD [28]. They also affect the probability of a successful ignition and combustion performance (such as BR and LI) of a composition [27,29,30].…”
Section: Effect Of Binder Content On the Fs LI And Br Of Mg/ba(no 3 )...mentioning
confidence: 99%
“…Therefore, they affect sensitivity to friction and ESD [28]. They also affect the probability of a successful ignition and combustion performance (such as BR and LI) of a composition [27,29,30].…”
Section: Effect Of Binder Content On the Fs LI And Br Of Mg/ba(no 3 )...mentioning
confidence: 99%
“…The gasless delay compositions main components are oxidizer, fuel and binder. The main role of oxidizer as chlorates and chromates is to supply the required amount of oxygen during combustion [5][6][7]. Large amount of heat can be secured during oxidation of fuel which considered one of the vital components of delay composition [8].…”
Section: Introductionmentioning
confidence: 99%
“…After heat and oxidative aging, the HTPB coating's cross-linked network is destroyed, and the mechanical properties will deteriorate [2]. At the same time, HTPB coating will be influenced by dynamic load during storage and transportation, and the frequency of loading will also impair the dynamic mechanical properties [3]. Under the interaction of thermal oxygen aging and dynamic load, it will significantly affect the operational performance of HTPB coating, and even cause fatal strike to solid rocket motor (SRM).…”
Section: Introductionmentioning
confidence: 99%