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Bicyclo-HMX as an Energetic Additive for Composite Propellants

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216275%3A25310%2F23%3A39920423" target="_blank" >RIV/00216275:25310/23:39920423 - isvavai.cz</a>

  • Result on the web

    <a href="https://doi.org/10.2514/1.B38977" target="_blank" >https://doi.org/10.2514/1.B38977</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.2514/1.B38977" target="_blank" >10.2514/1.B38977</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Bicyclo-HMX as an Energetic Additive for Composite Propellants

  • Original language description

    This paper deals with the ballistic parameters of composite propellants containing bicyclo-HMX (BCHMX) as an energetic additive. The results were compared with the same composite propellant containing HMX. On the basis of the results of the measurement using a Stojan vessel, it was found that the burning rates of BCHMX containing propellants are in most cases higher compared to HMX in propellants. Increasing the concentration of HMX in the propellant often leads to a decrease in burning rate. This trend was not observed for higher concentrations of BCHMX. The pressure exponent of all tested propellants is less than 1, whereby lower values were mostly observed for BCHMX propellant samples. Propellants containing BCHMX are also distinguished by easy ignitability. Using REAL software, it was found that propellants containing BCHMX achieve high specific impulses which, at BCHMX content in the propellant over 30 %, exceed the specific impulse values of the propellant without BCHMX content and all tested propellants containing HMX.

  • Czech name

  • Czech description

Classification

  • Type

    J<sub>imp</sub> - Article in a specialist periodical, which is included in the Web of Science database

  • CEP classification

  • OECD FORD branch

    10401 - Organic chemistry

Result continuities

  • Project

    <a href="/en/project/TH03020263" target="_blank" >TH03020263: Propellants with increased a specific impulse</a><br>

  • Continuities

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Others

  • Publication year

    2023

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Name of the periodical

    Journal of Propulsion and Power

  • ISSN

    0748-4658

  • e-ISSN

    1533-3876

  • Volume of the periodical

    39

  • Issue of the periodical within the volume

    4

  • Country of publishing house

    US - UNITED STATES

  • Number of pages

    6

  • Pages from-to

    626-631

  • UT code for WoS article

    000969777100001

  • EID of the result in the Scopus database

    2-s2.0-85163961565