Results 121 to 130 of about 849 (186)

Investigation of PBT-AP Interactions in PBT-Based Solid Propellants: A Combined Density Functional Theory and Molecular Dynamics Study. [PDF]

Polymers (Basel)
Liu K, Cheng X.
europepmc   +1 more source

Simulation of Aging and Bonding Properties of the Matrix/Filler Interface in Particle-Reinforced Composites. [PDF]

Polymers (Basel)
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]

Sci Rep
Yehia M, Ismael S, Naeem I, Sousa-Castillo A, Vázquez-González M, Correa-Duarte MA, Elbasuney S.   +6 more
europepmc   +1 more source

Fatigue failure of prefabricated crack HTPB(hydroxyl-terminated polybutadiene) propellant under strain control. [PDF]

Sci Rep
Li G, Gao B, Hu H, Cui R, Feng J, He J.
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Experimental and machine learning-driven assessment of IS 2062 steel under double-base propellant combustion conditions. [PDF]

Sci Rep
Singh H, Sundeep D, Sastry CC, Varadharaj EK.   +3 more
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Vortex cooled thermoplastic chamber thruster for potential application to polymer based 3D printed space propulsion systems. [PDF]

Sci Rep
Aqailan M, Huh J.
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A green stabilizer for Nitrate ester-based propellants: An overview. [PDF]

Heliyon
Rusly SNA, Jamal SH, Samsuri A, Mohd Noor SA, Abdul Rahim KS.   +4 more
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Acoustic Resonance in Solid Propellant Rockets

Journal of Applied Physics, 1960
Attention is drawn to the fact that the solid propellant must, in general, be considered as one of the acoustic media in a rocket motor. The viscoelastic properties of the solid along with those of the burned gases determine the characteristic modes of the system corresponding to the particular boundary conditions imposed on these media by the metal ...
McClure, F. T., Hart, R. W., Bird, J. F.
openaire   +2 more sources

Stabilization of a solid propellant rocket instability

Proceedings of the 40th IEEE Conference on Decision and Control (Cat. No.01CH37228), 2002
A globally stabilizing feedback boundary control law for an arbitrarily fine discretization of a one-dimensional nonlinear PDE model of unstable burning in solid propellant rockets is presented. The PDE has a destabilizing boundary condition imposed on one part of the boundary.
Dejan M. Boskovic, Miroslav Krstic
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