نتایج جستجو برای: propellant inhibitor

تعداد نتایج: 212760  

ژورنال: مواد پرانرژی 2011
فارغی علمداری, رضا, موسوی ندوشن, سید امان اله , هراتی, مرتضی,

  Abstract   In this work, the effects of quality and quantity of three stabilizers as AkarditeII, 2-NDPA and CentraliteI on the heat of explosion and stability of double-based is investigated The results showed that, by increasing the amount of AkarditeII and 2-NDPA increased stability of propellant and decreased heat of explosion. By replace AkarditeII and 2NDPA with CentraliteI and AkarditeI...

Journal: :International Journal of Aerospace Engineering 2018

Journal: :Gravitational and Space Research 2021

Journal: :Physics of Fluids 2021

The theoretical results of the present work reveal a significant interaction oncoming vortex ring propellant muzzle gases with backward blood spatter. It is shown that there even possibility droplet from backspatter will fully turn around by powerful and land behind victim. Such predicted outcome confirmed experimental data reversed drop trajectories observed in experiments conducted second par...

2006
c.

The interest in interplanetary space travel has stimulated much discussion on the desirability of using nuclear, rather than chemical, energy for the spacecraft propulsion. Comparisons of the relative merits of various propulsion systems have been extensively discussed in the literature. The results of such studies yield a diversity of conclusions, depending on the assumptions which are made in...

ژورنال: مواد پرانرژی 2015

In this study, the effect of Fe3O4-coated graphene as a nanocatalyst on the degradation kinetics of Ammonium Perchlorate and Glysydyl Azide Polymer (AP/GAP) composite propellants is investigated in order to modify and improve the burning rate of propellants. The SEM-EDX and EDX-Mapping surface analysis methods were used for structural and morphological study of the propellant containing nanoca...

Journal: :TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 2017

Journal: :International Conference on Aerospace Sciences and Aviation Technology 2003

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