The calculation of theoretical energetic performances of composite rocket propellants
A suitable method for calculating theoretical energetic performances of a composite propellant was investigated and successfully verified. This method is based on generally accepted hypotheses, consistent and simple calculation of the chemical equilibrium in a predominantly gaseous, multi-c...
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Serbian Chemical Society
2001-01-01
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doaj-81cadf1bd2f24ebda3fd7cf30b424ffa2020-12-24T07:34:51ZengSerbian Chemical Society Journal of the Serbian Chemical Society0352-51391820-74212001-01-0166210711710.2298/JSC0102107F0352-51390102107FThe calculation of theoretical energetic performances of composite rocket propellantsFilipović Miloš0Kilibarda Nikola1Military Technical Institute, BelgradeMilitary Technical Institute, BelgradeA suitable method for calculating theoretical energetic performances of a composite propellant was investigated and successfully verified. This method is based on generally accepted hypotheses, consistent and simple calculation of the chemical equilibrium in a predominantly gaseous, multi-component reactive mixture, and on an appropriate numerical scheme involving the propellant formula and the assigned rocket motor operating conditions. Acomputer program, which permits the calculation of the equilibrium composition of the combustion products and the theoretical energetic performances of composite propellants has been developed. The results of the calculations have been compared with data obtained by the programs OPHELIE, MICROPEP, and the program SPP, as documented in the NASA-Lewis Code, which is presently a world-wide standard. All comparisons gave satisfactory agreement.http://www.doiserbia.nb.rs/img/doi/0352-5139/2001/0352-51390102107F.pdfcomposite propellantscombustioncombustion productschemical equilibriumtheoretical energetic performances |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Filipović Miloš Kilibarda Nikola |
spellingShingle |
Filipović Miloš Kilibarda Nikola The calculation of theoretical energetic performances of composite rocket propellants Journal of the Serbian Chemical Society composite propellants combustion combustion products chemical equilibrium theoretical energetic performances |
author_facet |
Filipović Miloš Kilibarda Nikola |
author_sort |
Filipović Miloš |
title |
The calculation of theoretical energetic performances of composite rocket propellants |
title_short |
The calculation of theoretical energetic performances of composite rocket propellants |
title_full |
The calculation of theoretical energetic performances of composite rocket propellants |
title_fullStr |
The calculation of theoretical energetic performances of composite rocket propellants |
title_full_unstemmed |
The calculation of theoretical energetic performances of composite rocket propellants |
title_sort |
calculation of theoretical energetic performances of composite rocket propellants |
publisher |
Serbian Chemical Society |
series |
Journal of the Serbian Chemical Society |
issn |
0352-5139 1820-7421 |
publishDate |
2001-01-01 |
description |
A suitable method for calculating theoretical energetic performances of a
composite propellant was investigated and successfully verified. This method
is based on generally accepted hypotheses, consistent and simple calculation
of the chemical equilibrium in a predominantly gaseous, multi-component
reactive mixture, and on an appropriate numerical scheme involving the
propellant formula and the assigned rocket motor operating conditions.
Acomputer program, which permits the calculation of the equilibrium
composition of the combustion products and the theoretical energetic
performances of composite propellants has been developed. The results of the
calculations have been compared with data obtained by the programs OPHELIE,
MICROPEP, and the program SPP, as documented in the NASA-Lewis Code, which
is presently a world-wide standard. All comparisons gave satisfactory
agreement. |
topic |
composite propellants combustion combustion products chemical equilibrium theoretical energetic performances |
url |
http://www.doiserbia.nb.rs/img/doi/0352-5139/2001/0352-51390102107F.pdf |
work_keys_str_mv |
AT filipovicmilos thecalculationoftheoreticalenergeticperformancesofcompositerocketpropellants AT kilibardanikola thecalculationoftheoreticalenergeticperformancesofcompositerocketpropellants AT filipovicmilos calculationoftheoreticalenergeticperformancesofcompositerocketpropellants AT kilibardanikola calculationoftheoreticalenergeticperformancesofcompositerocketpropellants |
_version_ |
1724372107774656512 |