Results 41 to 50 of about 210 (122)
Study of Energetic Nitramine Extruded Double-Base Propellants [PDF]
, 2013 This paper gives the results of an experimental study on nitramine extruded double-base (EDB)fonnulationscontaining up to 25 percent RDXin low and high calorimetric value double-base(DB)propellants.
Gautam, G. K. +4 more
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Nitramine-Based High Energy Propellant Compositions for Tank Guns [PDF]
, 2013 Six different RDX-based gun propellant compositions have been formulated and studied to select the most suitable composition for tank gun ammunition in terms of higher force constant at relatively lower flame temperature (T). Ballistic'performance of the
Damse, R.S., Singh, Haridwar
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A Review of the Catalytic Effects of Lead‐Based Ballistic Modifiers on the Combustion Chemistry of Double Base Propellants [PDF]
, 2020 Lead‐based compounds are the current industry‐standard ballistic modifier for double‐base propellants, but there is a pressing need for alternatives as incoming European legislation will soon ban their use.
An T. +10 more
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Modelling of DMNB Content for Marked Plastic Explosives [PDF]
, 2007 2,3-dimethyl-2,3-dinitrobutane (DMNB) has been internationally accepted as an additive forthe purpose of marking, as it has desired vapour pressure for reliable detection.
A. Subhananda Rao +4 more
core +2 more sources
Synthesis and Characterisation of Poly (aminotrinitrophenylene) [PDF]
, 2013 Poly(amipotrinitrophenylene) (PATNP), a thermally-stable explosive has been synthesisied by ring amination of polynitropolyphenylene (PNP) using hydroxylamine hydrochloride in dimethyl formamide in the presence of alcoholic KOH.
Malwade, M.S. +2 more
core +2 more sources
Metallised Fuel rich Propellants for Solid Rocket Ramjet: A Review [PDF]
, 2013 This paper reviews the research work carried out in the field of metallised fuel-rich propellants (FRP). Limitations and merits of various potential metals (Al, Mg, B, Be, or Zr) as a component of FRP are discussed.
Asthana, S. N. +2 more
core +2 more sources
Solid rocket motor internal insulation [PDF]
Internal insulation in a solid rocket motor is defined as a layer of heat barrier material placed between the internal surface of the case propellant.
Keller, R. B., Jr., Twichell, S. E.
core +1 more source
A Survey: Destruction of Chemical Agent Simulants in Supercritical Water Oxidadtion [PDF]
, 1992 U.S.
Blank, M.R., Gloyna, E.F.
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, 2023 Abstract In order to predict the storage life of composite modified double base propellant (CMDB propellant) at 298.15K, the correlation between the maximum elongation and the stabilizer depletion of CMDB propellant was studied. The thermal accelerated aging tests were carried out at 323.15K, 333.15K, 343.15K and 353.15K.
Jia-ming Liu +4 more
openaire +1 more source
A Reliable Method for Predicting the Specific Impulse of Chemical Propellants
Journal of Aerospace Technology and Management, 2018 The specific impulse (Isp) is an important performance parameter that describes energy efficiency of propellant combustion and is intimately related to the rocket engine thrust.
Dany Frem
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