Results 21 to 30 of about 412,817 (220)
Agglomerate Size Evolution in Solid Propellant Combustion under High Pressure
Aerospace, 2023 Solid propellant combustion and flow are significantly affected by condensed combustion products (CCPs) in solid rocket motors. A new aluminum agglomeration model is established using the discrete element method, considering the burning rate and ...
Songchen Yue +7 more
doaj +1 more source
Interaction of LOX/GH2-Spray Combustion with Acoustics [PDF]
, 2007 The response of a cryogenic LOX/H2-spray flame to acoustic pressure and velocity fluctuations has be investigated experimentally for pressure levels up to p=1MPa.
Bernhard Knapp +5 more
core +1 more source
Sublimation of ice particles from rocket exhausts in the upper atmosphere [PDF]
, 2003 The process of sublimation of ice particles from a rocket exhaust in the upper atmosphere is examined. Heating by solar radiation and losses of energy by means thermal radiation and sublimation are taken into account in the thermal balance of the ice ...
Kosch, Mike J., Platov, Y. V.
core +4 more sources
Rocket Motor with Composite Casing [PDF]
Problemy Mechatroniki, 2015 The article presents the results of work concerning a two-stage rocket motor. In the first step tested stationary the charge rocket motor with the ignitor and the nozzle system in the ballistic chamber was tested.
Zbigniew Drabik, Tomasz Rasztabiga
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Combustion Chamber Acoustics and its Interaction with LOX/H2- and LOX/CH4-Spray Flames [PDF]
, 2008 The acoustics of combustion chambers and the interaction of acoustics and combustion is investigated in a model combustor operated with LOX/H2 and LOX/CH4.
Marpert, Marl +5 more
core +1 more source
A Study on Dynamic Characteristics of Thin-Walled Cylindrical Cavities with a Large Aspect Ratio
Aerospace, 2022 The unstable combustion problem in small-sized solid rocket engines with a large aspect ratio is so complicated that its causes remain unclear. In this study, the coupled vibration between the sound field and shell in the engines was proposed as a ...
Fangfang Xu, Hong Li, Dongxu Zhang
doaj +1 more source
FirePhysChem, 2021 Human spaceflight, space tourism, and the launch of microsatellites are all expected to grow in the future. In fact, with the recent increase of the satellite market, almost 1000 smallsats per year are foreseen to be launched over the next decade. Hybrid
Yash Pal +4 more
doaj +1 more source
Large-Eddy Simulation of combustion instabilities in a variable-length combustor. [PDF]
, 2013 This article presents a simulation of a model rocket combustor with continuously variable acoustic properties thanks to a variable-length injector tube. Fully compressible Large-Eddy Simulations are conducted using the AVBP code.
Garby, Romain +5 more
core +1 more source
Laser induced fluorescence thermometry with OH (2, 0) band excitation
Journal of Fluid Science and Technology, 2016 Measurement technique that can be adapted to high temperature and pressure environment in the rocket combustion chamber has been limited to qualitative.
Teppei YANO +3 more
doaj +1 more source
Effects of Compounds in Liquefied Methane on Rocket Engine Operation
Aerospace, 2022 Methane (CH4) is a promising rocket fuel for various future space mission scenarios. It has advantages in terms of cost, performance, and environmental friendliness.
Jan van Schyndel +4 more
doaj +1 more source