Results 181 to 190 of about 7,767 (239)

Damage characteristics and failure mechanism analysis of NEPE propellant at high strain rates. [PDF]

Sci Rep
Sun Z, Xu J, Zhou C, Chen X, Guo Z, Song Q.   +5 more
europepmc   +1 more source

Study on rheological properties of composite propellant slurry in the mixing process by using experimental and numerical simulation. [PDF]

RSC Adv
Guo Z, Fu X, Rossi R.
europepmc   +1 more source

Mesoscale Damage Evolution, Localization, and Failure in Solid Propellants Under Strain Rate and Temperature Effects. [PDF]

Polymers (Basel)
Gao B, Xiao Y, Yu W, Qu K, Sun Y.
europepmc   +1 more source

Detection of Debonding Defects in Carbon Fiber-Reinforced Polymer (CFRP)-Rubber Bonded Structures Based on Active Lamb Wave Energy Analysis. [PDF]

Sensors (Basel)
Yang Z, Ren Y, Shi Q, Cui D, Liu J.
europepmc   +1 more source

Research on Crack Propagation of Nitrate Ester Plasticized Polyether Propellant: Experiments and Simulation. [PDF]

Materials (Basel)
Liu H, Wang J, Fu X.
europepmc   +1 more source

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

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Energetic water compositions as rocket propellants

Acta Astronautica, 2021
Abstract New results of experimental and theoretical research of ignition and combustion of energetic water compositions used as environmentally safe (green) propellants for rocket and other internal combustion engines are presented. The theoretical assessment of the thermodynamic effect of water additives to fuels depending on the characteristics of
Igor G. Assovskiy, Genadiy P. Kuznetsov, Georgiy V. Melik-Gaikazov   +2 more
openaire   +1 more source

Nano-composites for rocket solid propellants

Composites Science and Technology, 2005
Aim 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 ...
MEDA, LUISA MARINA, G. Marra, GALFETTI, LUCIANO, DE LUCA, LUIGI, F. Severini, S. Inchingalo   +5 more
openaire   +2 more sources

Burning of Nano-Aluminized Composite Rocket Propellants

Combustion, Explosion and Shock Waves, 2005
Several aluminum nanopowders were examined and compared with the final goal to evaluate their application in solid rocket propulsion. A detailed investigation of pre-burning properties by the Brunauer-Emmet-Teller method, electron microscopy, X-ray diffraction, and X-ray photoelectron spectroscopy was carried out.
DE LUCA, LUIGI, GALFETTI, LUCIANO, F. Severini, L. Meda, G. Marra, A. Vorozhtsov, V. Sedoi, V. Babuk   +7 more
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Combustion of composite solid rocket propellants.

AIAA Journal, 1969
CONSIDERABLE work has been done on solid rocket ^->< propellants using various fuels (often polymers) and oxidizers. Recently Rastogi and Ouseph have studied the combustion of phenol-f ormaldehy de/NH 4C10 4 system . They observed that the rate of burning decreases as the amount of cross-linking increases in the polymer.
R. P. RASTOGI, B. L. GUPTA
openaire   +1 more source