Results 191 to 200 of about 907 (260)

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.
europepmc   +1 more source

Circular Economy Pathways for Airport Climate Change Mitigation

Business Strategy and the Environment, EarlyView.
ABSTRACT Airport operators face growing climate‐change pressures; the circular economy offers pathways to reduce impacts and recover resources. We examine how airport operators apply the circular economy in practice. We use an exploratory qualitative multicase design based on practitioner‐generated documents (e.g., press releases and sustainability ...
Michele Oppioli, Davide Calandra, Federico Lanzalonga, Paolo Biancone   +3 more
wiley   +1 more source

Floatable Syntactic Magnesium Foam as a Marangoni-Induced Propulsion Microboat. [PDF]

Materials (Basel)
Thalmaier G, Sechel NA, Vida-Simiti I.
europepmc   +1 more source

First applications of ultrasound technology in solid rocket propellant combustion promotion. [PDF]

Ultrason Sonochem
Wen Z, Jing H, Hao F, Wang Y, Kuang B, Liu P, Ao W.   +6 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

Molecular Simulations of Interface-Driven Crosslinked Network Formation and Mechanical Response in Composite Propellants. [PDF]

Polymers (Basel)
Ling C, Zhang X, Li X, Mou G, Guo X, Yuan B, Yang K.   +6 more
europepmc   +1 more source

Review of Recent Advances in Cold-Sprayed Coatings for Accident-Tolerant Fuel Cladding. [PDF]

Materials (Basel)
Mou Y, Zhou Y, Zhou H, Yang R, Huang J, Tian Y, Wu S, Zhou P, Song M, Han J, Li H.   +10 more
europepmc   +1 more source

Research on Curing Reaction Kinetics and Curing Process of Nitrate Ester Plasticized Polyether (NEPE) Propellants. [PDF]

Polymers (Basel)
Wu Y, Guo Z, Yu H, Fu X.
europepmc   +1 more source

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Detonability of Solid Composite Propellants

ARS Journal, 1961
The 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.
openaire   +2 more sources

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