A Reliable Method for Predicting the Specific Impulse of Chemical Propellants
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
doaj
Improving the Combustion Efficiency of Aluminum-Based Composite, Al@IL/FG, Through Surface Activation Reaction. [PDF]
Zheng QL, Huang ZL, Xu HX, Li JZ, He W.
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A Physics-Informed Manifold Neural Operator Framework for Multi-Parameter Prediction of Polymer Aging in HTPB Solid Propellants. [PDF]
Liu S +5 more
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Meso-Scale Observations of the Evolution of Matrix/Filler Interface Dewetting During NEPE Propellant Aging. [PDF]
Chen Z +5 more
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Correction: Research on curing reaction kinetics and curing process of hydroxy-terminated polybutadiene (HTPB) propellants. [PDF]
Guo Z +7 more
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A Method for Reducing the Temperature Sensitivity of a Single-Base Propellant by Adding Ultra-Fine RDX Particles. [PDF]
Zhu S +9 more
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A Breath of Fresh Air: Carbon Emissions From Inhaler Devices and the Role of Prescribing Clinicians in Reducing Their Environmental Harm. [PDF]
Ahmed JI.
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Ensuring continued access to essential inhaled respiratory medications: a call to action from the Inhaled Respiratory medicine Innovation and environmental Sustainability (IRIS) group. [PDF]
Hurst JR +11 more
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Study on Creep Mechanical Properties of HTPB Solid Propellant. [PDF]
Jin L, Jia S, Zhang Z, An Z, Lu Z.
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Global pMDI Use and the Potential Impact of European PFAS Legislation on Access to These Essential Inhaled Medications. [PDF]
Kocks JWH +5 more
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