8th Symposium on Space Resource Utilization 2015
DOI: 10.2514/6.2015-1653
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Feasibility of high speed atmospheric flight on Venus

Abstract: Exploring Venus is difficult, so far, probes have managed to survive only few hours. However, Venus' atmosphere, composed of 96.5 % CO2 might provide an unique opportunity for a airbreathing vehicle. In this context, this paper intends to study the feasibility of a scramjet/ramjet engine for flying in Venus' atmosphere at an altitude of ~70 km. The first part of the work focuses on the choice of fuel. The most promising candidates to burn in CO2 are metals and their hydrides. In this context, the analysis of a… Show more

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“…Many of these studies have been coupled with preliminary hybrid rocket engine or component design, assessing methods for particle transport and dispersion as well as engine configuration [2,5]. The potential benefits of CO 2 -Mg(s) have also been addressed, being incorporated into various mission concepts [2,3,10,11]. Lastly, the feasibility of CO 2 -Mg(s) has been demonstrated, with both rocket and turbojet engines being built and successfully producing thrust [12,13] for abbreviated periods of time.…”
Section: Historical Work Surveymentioning
confidence: 99%
“…Many of these studies have been coupled with preliminary hybrid rocket engine or component design, assessing methods for particle transport and dispersion as well as engine configuration [2,5]. The potential benefits of CO 2 -Mg(s) have also been addressed, being incorporated into various mission concepts [2,3,10,11]. Lastly, the feasibility of CO 2 -Mg(s) has been demonstrated, with both rocket and turbojet engines being built and successfully producing thrust [12,13] for abbreviated periods of time.…”
Section: Historical Work Surveymentioning
confidence: 99%