Jump to main content
US EPA
United States Environmental Protection Agency
Search
Search
Main menu
Environmental Topics
Laws & Regulations
About EPA
Health & Environmental Research Online (HERO)
Contact Us
Print
Feedback
Export to File
Search:
This record has one attached file:
Add More Files
Attach File(s):
Display Name for File*:
Save
Citation
Tags
HERO ID
8278439
Reference Type
Journal Article
Title
Energetic abilities of solid composite propellants based on 3, 4, 5-trinitropyrazole and ammonium dinitramide
Author(s)
Lempert, DB; Chukanov, N; Shu, YJ
Year
2016
Publisher
China Ordnance Industry Corporation
Volume
39
Issue
3
Page Numbers
17-20
Language
English
DOI
10.14077/j.issn.1007-7812.2016.03.003
Abstract
The investigation aims at the expansion of the basis of formulations of solid composite propellants by introducing new compositions with lower sensitivity to mechanic impact and improved thermal stability. The formulations based on trinitropyrazole (TNP) contains a binder (a hydrocarbon or active one), aluminum and inorganic oxidizer ADN. The results show that a binary formulation TNP + active binder (18%-19%)(volume fraction) with no metal is well designed which would achieve high specific impulse (at Pcâ¶Pa=40â¶1) of 248 s, high density of 1.80 g/cm3 and combustion temperature Tc about 3450 K. In terms of energy, metal-free compositions with TNP lose a bit to those with HMX, only if HMX fraction in formulation is higher than 45%-50%. © 2016, Editorial Board of Journal of Explosives & Propellants. All right reserved.
Keywords
3, 4, 5-trinitropyrazole; ADN; Ammonium dinitramide; Binder; Solid composite propellants; Specific impulse; TNP
Home
Learn about HERO
Using HERO
Search HERO
Projects in HERO
Risk Assessment
Transparency & Integrity