Two-pulse Solid Propellant Rocket Motor Solution

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F15%3A00531883" target="_blank" >RIV/60162694:G43__/15:00531883 - isvavai.cz</a>
Result on the web
<a href="http://vavtest.unob.cz/registr" target="_blank" >http://vavtest.unob.cz/registr</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1109/MILTECHS.2015.7153747" target="_blank" >10.1109/MILTECHS.2015.7153747</a>

Result language
angličtina
Original language name
Two-pulse Solid Propellant Rocket Motor Solution
Original language description
Mathematic simulation of dynamic processes in two pulse solid propellant rocket motor is presented. The dynamic approach to the solution is formed by the ordinary differential equations of the mass and energy conservation laws in gas flow. Pressure and thrust courses are used for the solution results demonstration.
Czech name
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Czech description
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Project
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year
2015
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
International conference on Military Technology 2015
ISBN
978-80-7231-976-3
ISSN
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e-ISSN
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Number of pages
5
Pages from-to
49-53
Publisher name
Faculty of Military Technology, Univerzity of Defence
Place of publication
Brno
Event location
Brno
Event date
May 19, 2015
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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