Prospects for the mastery of space and the basic problems which must be solved in developing systems for both manned and cargo spacecraft are examined. The achievements and flaws of rocket boosters are discussed as well as the use of reusable spacecraft.
Chekalin, S. V., Grishin, S. D.
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Investigation of liquid rocket swirl coaxial injection dynamics under self-excited high frequency oscillations [PDF]
, 2016 Liquid-centered swirl coaxial injector elements used within liquid rocket combustion devices can exhibit self-excited and self-sustained oscillations known commonly as self-pulsations.
Eberhart, Chad Jonathan
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"MARKS" SMALL AVIATION-ROCKET SPACE LAUNCH SYSTEM [PDF]
, 2018 The problems of delivery of small space vehicles into low earth orbits are pointed out. The up-to-date means for the ascent of small space vehicles into low earth orbits are analysed.
A. V. KORNEV +3 more
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Scaling of Performance in Liquid Propellant Rocket Engine Combustors [PDF]
, 2007 This paper discusses scaling of combustion and combustion performance in liquid propellant rocket engine combustion devices. In development of new combustors, comparisons are often made between predicted performance in a new combustor and measured ...
Hulka, James R.
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Injection systems of rocket engines [PDF]
, 2021 Tato bakalářská práce se zabývá konstrukcí trysek raketového motoru na kapalné látky. Teoretická část popisuje dělení do skupin a princip funkce raketových trysek.
Vrbica, Kryštof
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Assessing Spontaneous Combustion Instability with Nonlinear Time Series Analysis [PDF]
Considerable interest lies in the ability to characterize the onset of spontaneous instabilities within liquid propellant rocket engine (LPRE) combustion devices.
Casiano, M. J., Eberhart, C. J.
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On the atomization behavior of Newtonian fluids with an impinging jet injector [PDF]
, 2010 LAUREA SPECIALISTICANel presente laovoro sono state studiate sperimentalmente le caratteristiche di atomizzazione di una vasta gamma di fluidi Newtoniani mediante l'utilizzo di impinging jet injector, in condizioni standard ed in pressione.
BAILARDI, GIOVANNI
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МАТЕМАТИЧНА МОДЕЛЬ ГАЗОПРОВОДУ ПНЕВМАТИЧНИХ СИСТЕМ РАКЕТНИХ ДВИГУНІВ ЯК СИСТЕМИ З ЗОСЕРЕДЖЕНИМИ ПАРАМЕТРАМИ [PDF]
Gas pipelines are key elements in systems for transporting and supplying compressed gas in various technical systems, including supercharging fuel tanks of liquid rocket engines and other pneumatic systems.
Alieksieienko, V. G., Bucharskyi, V. L.
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Cooperative Development of L75 LOX Ethanol engine: Current Status with Focus on Capacitive Chamber Testing [PDF]
, 2016 In 2011 DLR and AEB agreed to cooperate in the field of liquid propulsion. The L75 engine project, which started in 2008 in Brazil, is the focus of this effort.
Burkhardt, Holger +6 more
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Thermo-Structural analysis of rocket engine thrust chamber [PDF]
, 2018 The rocket engine market today presents several new trends that will substantially change the current technological scenario. Apart from the imminent applications to the mega constellations and the advancement of electric propulsion, some aspects such as
Madhu Suryavanshi, Chethan
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