Searched for: subject%3A%22pressure%255C-fed%22
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Hermsen, R.J.G. (author)
To launch a rocket to the edge of space using a pressure fed rocket system with liquid oxygen as propellant, you need to know exactly how much pressurant gas (helium) you need to take along. In this thesis a practical investigation on cryogenic tank pressurization is conducted together with DARE. The measurement results are used to validate...
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