Results 41 to 50 of about 49,027 (122)
Size and Shape of Ammonium Perchlorate and their Influence on Properties of Composite Propellant [PDF]
, 2009 Most of the composite propellant compositions contain solid loading up to 86 per cent. The main solid ingredients of composite propellant are ammonium perchlorate (AP) and aluminium powder.
Bhattacharya, B. +5 more
core +2 more sources
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
core +2 more sources
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
core +2 more sources
Studies on Stress-Strain Curves of Aged Composite Solid Rocket Propellants [PDF]
, 2012 Mechanical property evaluation of composite solid rocket propellants is used as a quick quality control tool for propellant development and production. However, stress-strain curves from uni-axial tensile testing can be utilised to assess the shelf-life ...
Shekhar, Himanshu
core +2 more sources
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
core +2 more sources
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
, 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