Results 101 to 110 of about 888 (231)
Ignition and combustion of high-energy materials containing aluminum, boron and aluminum diboride
MATEC Web of Conferences, 2018 Boron and its compounds are among the most promising metal fuel components to be used in solid propellants for solid fuel rocket engine and ramjet engine.
Korotkikh Alexander +2 more
doaj +1 more source
Blistering barnacles: Space physiology in The Adventures of Tintin
Experimental Physiology, EarlyView.
Jacob P. Hartmann +4 more
wiley +1 more source
, 1969 Refractory metal and graphite composite research for solid propellant rocket nozzle ...
Manning, C. R., Jr., Lineback, L. D.
core +1 more source
Review on typical ingredients for ammonium perchlorate based solid propellant [PDF]
, 2015 Ammonium perchlorate (AP) based solid propellant is a modern solid rocket propellant used in various applications. The combustion characteristics of AP based composite propellants were extensively studied by many research scholars to gain higher thrust ...
Wan Ali, Wan Khairuddin +7 more
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3-D grain burnback analysis of solid propellant rocket motors: Part 1-ballistic motor tests
, 2008 The performance prediction of solid rocket motors is an important phase during the design process and it can be achieved easily if the burnback steps of the solid propellant are known.
Puskulcu, G., Ulaş, Abdullah
core +1 more source
Nonideal detonation and initiation behavior of a composite solid rocket propellant. [HMX/AP/Al]
, 1981 Shock initiation and detonation behavior of an HMX/AP/Al rocket propellant were studied for nonideal character. Low detonation velocities and unusual shock initiation behavior were observed.
Dick, J. J.
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Performance of composite solid rocket propellants for rocket assisted projectiles (RAP) [PDF]
The International Conference on Chemical and Environmental Engineering, 2016 Mohamed Nawwar +2 more
openaire +1 more source
Journal of Aerospace Technology and Management, 2012 Rockets are powered by composite solid propellant, which is a heterogeneous system consisting of solid oxidizer and metallic fuel dispersed in a polymeric fuel binder matrix.
Praveen Prakash Singh +5 more
doaj
Low flux radiative ignition studies of ammonium perchlorate composite propellants
, 2010 The vast majority of propellant ignition data has been collected and studied for heat fluxes in the typical, intentional ignition range. However, when a propellant contained within a rocket motor case is exposed to low fluxes in hazardous situations ...
Polo, Matt J.
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Pressure casting of composite propellant
, 2008 420-423Conventional vacuum casting technique is suitable only to propellant slurry with low viscosity (
Dombe, Ganesh +4 more
core