Searched for: subject%3A%22Liquid%255C%2BRocket%255C%2BEngine%22
(1 - 5 of 5)
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Kerstens, Fabio (author)
As a part of a <i>Future Launcher Preparatory Programme</i> contract issued by the European Space Agency, the aerospace startup company Dawn Aerospace is developing an integral, additive manufactured (AM), liquid rocket engine. This 2.5 kN class engine is propelled by the storable propellants 90% hydrogen peroxide and kerosene and used in the...
master thesis 2021
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Kerstens, Fabio (author), Cervone, A. (author), Gradl, P.R. (author)
High performance liquid rocket engines require cooling to maintain structural integrity of the combustion chamber which is exposed to high thermal and environmental loads. For many systems, this is achieved by means of regenerative cooling, where a coolant flows through passages around the chamber wall whilst extracting heat from the wall. A...
journal article 2021
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Nosseir, A.E.S. (author), Cervone, A. (author), Pasini, A (author)
Innovation in small-satellite modern space missions and applications require propulsion capabilities to enable active operations in orbit, such as formation flying, rendezvous operations, orbital altitude &amp; inclination changes, and orbital transfers,– generally, operations demanding high-thrust impulsive maneuvers. In addition, Green...
conference paper 2020
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Mercieca, Edward (author)
In Liquid Rocket Engine (LRE) design, knowledge of how the propellant atomization quality varies with respect to some injector design variables would be useful in predicting LRE performance. Three spray characteristics were chosen as a measure of Atomization quality: the Sauter Mean Diameter (SMD), the drop size distribution, and the cone angle....
master thesis 2017
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Ernst, R.R.L. (author)
The need to increase specific impulse of rocket launcher engines has lead design engineers to start development of ever more complex engine cycles starting from simple gas pressure fed engines to the very complex staged combustion cycle engines. Currently a wide range of different cycles does exist. These cycles not only differ in terms of...
master thesis 2014
Searched for: subject%3A%22Liquid%255C%2BRocket%255C%2BEngine%22
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