Results 61 to 70 of about 875 (223)

National Policy Coherence Counts for Reducing Inequality in Global Climate and Development Agendas

open access: yesSustainable Development, EarlyView.
ABSTRACT International institutions promote policy coherence as crucial to the effective and fair implementation of global sustainability agendas, though the evidence for its benefits is slim. We present here the first systematic cross‐country dataset on the consequences of national government efforts to promote policy coherence for vulnerable groups ...
Katherine Browne   +10 more
wiley   +1 more source

Chemical Reactor Network for Hybrid Rocket Engines Optimization [PDF]

open access: yes
This study proposes the integration of a chemical reactor network into the design optimization procedure of hybrid rocket engines. The adoption of a chemical reactor network enables a more realistic representation of combustion phenomena compared to ...
Lorenzo Folcarelli   +2 more
core   +1 more source

Theoretical prediction of regression rates in swirl-injection hybrid rocket engines [PDF]

open access: yes, 2016
The authors theoretically and analytically predict what times regression rates of swirl injection hybrid rocket engines increase higher than the axial injection ones by estimating heat flux from boundary layer combustion to the fuel port.
K. Ozawa, T. Shimada
core   +1 more source

Characterization and manufacturing of a paraffin wax as fuel for hybrid rockets

open access: yesPropulsion and Power Research, 2018
The hybrid propulsion performed with paraffin waxes exhibits most attractive capabilities compared to solid or liquid engines, e.g., throttleability and re-ignition, alongside higher regression rates compared to the conventional hydroxyl terminated ...
F. Piscitelli   +4 more
doaj   +1 more source

Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades

open access: yesVirtual and Physical Prototyping, 2023
Hybrid rocket engines suffer from the restricted mechanical properties and low regression rates of current polymeric fuel grains. We propose a three-dimensional printed aluminium (Al) nested composite fuel grain with millimetre-scale lattice pores ...
Dandan Qu   +9 more
doaj   +1 more source

Small‐Scale Magnetic Soft Robots for Medical Applications: From Laboratory to Clinical Use

open access: yesSmartBot, EarlyView.
Small‐scale magnetic soft robots are emerging as promising platforms for minimally invasive diagnosis and therapy in complex in vivo environments. This review compares untethered and tethered medical magnetic robots in parallel across five translational stages, from basic performance testing to clinical evaluation.
Xingxing Ke   +29 more
wiley   +1 more source

Combustion Processes in Hybrid Rocket Engines [PDF]

open access: yes, 1996
In recent years, there has been a resurgence of interest in the development of hybrid rocket engines for advanced launch vehicle applications. Hybrid propulsion systems use a solid fuel such as hydroxyl-terminated polybutadiene (HTPB) along with a ...
Merkle, C. L., Venkateswaran,S.
core   +1 more source

Strategy for One‐Step Optimization of Metal Oxide Passivating Contact Materials for Si Heterojunction Solar Cells through Growth Angle Variation

open access: yesSmall, EarlyView.
A one‐step oblique angle reactive sputtering approach enables simultaneous tuning of bulk and interfacial stoichiometry in a metal oxide/ silicon heterojunction. In case of vanadium oxides, growth angle variation controls the formation of stoichiometric SiO2, ternary SiOx(V) interlayer, and phase purity of vanadium oxide, considerably simplifying the ...
Aparajita Mandal   +3 more
wiley   +1 more source

One-Dimensional simulation of internal ballistic of a Hybrid Rocket Engine [PDF]

open access: yesعلوم، فناوری و کاربردهای فضایی
A one-dimensional code was developed to simulate the performance of hybrid rocket engines. In this code, the conservation equations of mass, momentum and energy are solved in one-dimensional and inviscid form.
Hadi Rezaei
doaj   +1 more source

Oxygen–Methane Torch Ignition System for Aerospace Applications

open access: yesAerospace, 2020
A new ignition system, based on a CH4/O2 torch has been developed by the Chemical Propulsion Laboratory of the University of Brasilia. Designed to ignite a hybrid rocket, this device has been improved to be used in testing of solid and liquid ramjet ...
Olexiy Shynkarenko, Domenico Simone
doaj   +1 more source

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