Results 161 to 170 of about 10,741 (228)

Rate-Dependent Tensile Properties of Aluminum-Hydroxide-Enhanced Ethylene Propylene Diene Monomer Coatings for Solid Rocket Motors. [PDF]

Materials (Basel)
Wang R, Zhang Y, Wang N, Wu Y.
europepmc   +1 more source

Pollution Effects and Management of Orbital Space Debris. [PDF]

ACS Omega
Shareefdeen Z, Al-Najjar H.
europepmc   +1 more source

Synthesis, Structure, Properties, and Applications of Fluorinated Polyurethane. [PDF]

Polymers (Basel)
Li D, Yu L, Lu Z, Kang H, Li L, Zhao S, Shi N, You S.   +7 more
europepmc   +1 more source

Effects of Thermal Damage on Impact Response Characteristics of High-Energy Propellants. [PDF]

Polymers (Basel)
Guo F, Nie J, Zhang S, Liang J, Liu R, Zou Y, Han Y.   +6 more
europepmc   +1 more source

Enhancing the landing guidance of a reusable launch vehicle by improving genetic algorithm-based deep reinforcement learning using Hybrid Deterministic-Stochastic algorithm. [PDF]

PLoS One
Nugroho L, Andiarti R, Akmeliawati R, Wijaya SK.   +3 more
europepmc   +1 more source

Combustion Enhancement of Gel Propellant Containing High Concentration Aluminum Particles Based on Carbon Synergistic Effect. [PDF]

Gels
Chen J, Zhao H, Li W, Liu H.
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Surface interactions and radical generation in TCD decomposition: a DFT approach. [PDF]

J Mol Model
Knoth SE, Tunega D, Aquino AJA.
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Liquid-Propellant Rocket Engine Injector Dynamics

Journal of Propulsion and Power, 1998
The dynamic characteristics of liquid-rocket injectors in the presence of intense combustion-chamber and propellant feed-line oscillations are discussed. Liquid-propellant injectors always function in nonsteady e ow environments and are therefore considered as a dynamic component of an engine.
Vigor Yang
exaly   +2 more sources