Results 61 to 70 of about 31,065 (215)
Defence Technology, 2016 A 30 mm electrothermal-chemical (ETC) gun experimental system is employed to research the burning rate characteristics of 4/7 high-nitrogen solid propellant.
Yan-jie Ni +5 more
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Steerable solid propellant rocket motor Patent [PDF]
, 1964 Steerable solid propellant rocket motor adapted to effect payload orientation as multistage rocket stage or reduce velocity as ...
Raggio, C. W., Jr.
core +1 more source
Nauka ta progres transportu, 2014 Purpose. Development of the operational numerical model to compute contamination of the atmosphere over Pavlograd city in the case of solid rocket propellant ignition at the storage. Methodology. To simulate the toxic chemical dispersion (product of the
M. M. Biliaiev +2 more
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Three-dimensional finite element analysis of acoustic instability of solid propellant rocket motors [PDF]
A three dimensional finite element solution of the acoustic vibration problem in a solid propellant rocket motor is presented. The solution yields the natural circular frequencies of vibration and the corresponding acoustic pressure mode shapes ...
Hackett, R. M., Juruf, R. S.
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Application of aluminum-based micro-cell composite fuel in HTPB propellant
Journal of Measurement Science and InstrumentationTo study the combustion performance of aluminum-based micro-cell composite fuel aluminum@ammonium perchlorate(Al@AP), in hydroxyl-terminated polybutadiene (HTPB) solid propellant, the Al@AP was added to HTPB solid propellant instead of Al powder and part
ZHOU Zhipeng +7 more
doaj
Dynamic Property Analysis of Electrically Controlled Solid Propellant
International Journal of Aerospace EngineeringThrough the dynamic mechanical analysis of lithium perchlorate/polyvinyl alcohol–based aluminized electrically controlled solid propellants, the temperature spectrum of the storage modulus (E′), loss modulus (E″), and loss factor (tan δ) of the ...
Zhicheng He, Jianjun Wu
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FirePhysChemSolid propellant fires, characterized by uncontrolled combustion behaviors, are a common occurrence in industries that utilize solid propellants and can lead to significant consequences. However, there has been a lack of comprehensive studies on modeling
Li Yu +4 more
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Long term investigation of bonding characteristics between PVC based inhibitor and HTPB/IPDI based propellant [PDF]
Scientific Technical ReviewBonding characteristics between extruded polyvinyl chloride (PVC) inhibitor and casted hydroxyl terminated polybutadiene/isophorone isocyanate (HTPB/IPDI) propellant, investigated in a long period of time, are topics of this paper. Basic statements about
Radulović Jovan, Milojković Aleksandar
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A nonlinear viscoelastic constitutive model with damage and experimental validation for composite solid propellant. [PDF]
Sci Rep, 2023 Li H, Xu JS, Chen X, Zhang JF, Li J.
europepmc +1 more source
Effects of Nano-Sized Al on the Combustion Performance of Fuel Rich Solid Rocket Propellants
Eurasian Chemico-Technological Journal, 2016 Several industrial- and research – type fuel rich solid rocket propellants containing nano-metric aluminum metal particles, featuring the same nominal composition, were prepared and experimentally analyzed. The effects of nano-sized aluminum (nAl) on the
W.Q. Pang +5 more
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