Results 11 to 20 of about 13,180 (230)
Numerical Analysis of Paraffin-Wax/Oxygen Hybrid Rocket Engines [PDF]
Journal of Propulsion and Power, 2020 A predictive numerical approach, based on Reynolds-averaged Navier–Stokes simulations including the effects of turbulence, chemistry, fluid/surface interaction, and radiation, has been developed fo...
Migliorino M. T., Bianchi D., Nasuti F.
openaire +4 more sources
Case Studies in Thermal EngineeringEffective cooling in rocket engines is essential to prevent overheating and ensure efficient performance under extreme operating conditions. This study presents a comprehensive investigation into advanced cooling strategies for rocket engines utilizing ...
Hatem Gasmi +7 more
doaj +3 more sources
Approaches to Low Fuel Regression Rate in Hybrid Rocket Engines
International Journal of Aerospace Engineering, 2012 Hybrid rocket engines are promising propulsion systems which present appealing features such as safety, low cost, and environmental friendliness. On the other hand, certain issues hamper the development hoped for.
Dario Pastrone
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CD8+ T cell memory is sustained in mice by hepatic stellate cells
Hepatology, EarlyView., 2022 HSC role in memory CD8+ T cell maintenance. Abstract Background and Aims Long‐lasting immunological memory is the ultimate goal of vaccination. Homeostatic maintenance of memory CD8+ cytotoxic T cells (MemCD8TCs) is thought to be mediated by IL‐15/IL‐15R heterodimer (15HD)‐expressing myeloid cells.
Yi‐Ting Chen +4 more
wiley +1 more source
Hybrid Rocket Engine Design Optimization at Politecnico di Torino: A Review
Aerospace, 2021 Optimization of Hybrid Rocket Engines at Politecnico di Torino began in the 1990s. A comprehensive review of the related research activities carried out in the last three decades is here presented.
Lorenzo Casalino +2 more
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DESIGN FEATURES OF ENGINES WITH PULSED DETONATION CAMERAS
Авіаційно-космічна техніка та технологія, 2020 The pressure of the products of chemical reactions in the chamber of a rocket engine increases significantly if the rocket fuel components burn in the detonation mode.
Олександр Євгенович Золотько +4 more
doaj +1 more source
Applied Sciences, 2023 A rocket’s turbulent jet radiates intense acoustic waves, which are an acoustic load for structural components like payload, launch structure, and rocket avionics, and impact communities near the launch site.
Giovanni Fasulo +4 more
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Optimal Design of Electrically Fed Hybrid Mars Ascent Vehicle
Aerospace, 2021 The optimal design of the propulsion system for a potential Mars Ascent Vehicle is analyzed, in the context of the Mars Sample Return Mission. The Mars Ascent Vehicle has to perform an initial ascent phase from the surface and then circularize into a 170
Lorenzo Casalino +2 more
doaj +1 more source
Ascent trajectory optimisation for a single-stage-to-orbit vehicle with hybrid propulsion [PDF]
, 2012 This paper addresses the design of ascent trajectories for a hybrid-engine, high performance, unmanned, single-stage-to-orbit vehicle for payload deployment into low Earth orbit. A hybrid optimisation technique that couples a population-based, stochastic
Brown, Richard +4 more
core +1 more source
Large-Scale CAMUI Type Hybrid Rocket Motor Scaling, Modeling, and Test Results
Aerospace, 2021 An understanding of the scalability of hybrid rocket regression models is critical for the enlargement and commercialization of small-scale engines developed within universities and similar research institutions.
Tor Viscor +4 more
doaj +1 more source