Numerical simulation of stability of diffusion depth of deterrents into cylindrical nitrocellulose composite under different conditions. [PDF]
Al-Hetty HRAK +3 more
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Advances and Challenges in Micro/Nanocarrier‐Based Dermal Drug Delivery Systems for Acne Treatment
Topical acne treatment faces challenges from skin barriers and complex causes. Micro/nanocarriers improve drug delivery by enhancing bioavailability, targeting, and duration. Combining carriers creates synergistic effects for systematic intervention.
Jintao Yang +7 more
wiley +1 more source
Amine-AlH<sub>3</sub> Adducts as Energetic Materials for a New Generation of Solid Fuels. [PDF]
Liu X +4 more
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Study on the Rheological Properties of BGAP Adhesive and Its Propellant. [PDF]
Shao Y +6 more
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Research on the influence of loading rate on the dynamic initiation fracture toughness of CMDB propellant. [PDF]
Zheng J +5 more
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Simulation of Aging and Bonding Properties of the Matrix/Filler Interface in Particle-Reinforced Composites. [PDF]
Chen Z, Wang X, Zou Z, Qiang H, Fu X.
europepmc +1 more source
Facile synthesis and decomposition kinetics of novel green energetic molecular perovskite based on nitrate group DAN-4 as an alternative for ammonium nitrate oxidizer. [PDF]
Yehia M +6 more
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Preparation of LaMn<sub>0.4</sub>Fe<sub>0.6</sub>O<sub>3</sub>/rGO composite catalyst for the thermolysis of ammonium perchlorate. [PDF]
Likhariya T, Dave PN.
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Detonability of Solid Composite Propellants
ARS Journal, 1961The thin film pla t inum resistance thermometer (heat flux gage) has been successfully applied to measurement of heat fluxes from initiators for solid propellants. Hea t fluxes measured were as high as 1000 Btu/ft-sec from hot, particleladen reaction products of pyrotechnic igniters.
Andersen, W. H., Chaiken, R. F.
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Nano-composites for rocket solid propellants
Composites Science and Technology, 2005Aim of this work is the study of different components (binder and aluminum powders) of solid propellants used for rocket propulsion to improve ballistic performance. New propellant formulations have been tested and characterised. Combustion residues were collected by a proprietary method and analyzed both from the morphological and chemical point of ...
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