Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Jonah E. Zimmerman"'
Publikováno v:
51st AIAA/SAE/ASEE Joint Propulsion Conference.
Nitrous oxide is frequently used as a self-pressurizing propellant in hybrid rocket propulsion systems. To study the behavior of these self-pressurized propellant tanks, two different pressure vessels with optical access have been developed that can
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::07dffe220aa5e5b30b465a775e4ca2ed
https://doi.org/10.2514/6.2015-3829
https://doi.org/10.2514/6.2015-3829
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Interest in nitrous oxide based hybrid rockets is at an all time high. Nitrous oxide (N2O) is a unique oxidizer because it exhibits a high vapor pressure at room temperature ( 730 psia or 5.03 MPa). Due to this high vapor pressure, liquid nitrous oxi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b49b19f4414dfa95974299e6cd85aa90
https://doi.org/10.2514/6.2014-3868
https://doi.org/10.2514/6.2014-3868
Publikováno v:
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Nitrous oxide is a popular oxidizer choice for many in the hybrid rocket community due to its ease of handling, storability at room temperature, and high vapor pressure. This high vapor pressure can be used as the pressurant, making it what is referr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5184d5fdf70de7e6d37c196bcb409403
https://doi.org/10.2514/6.2013-4045
https://doi.org/10.2514/6.2013-4045
Publikováno v:
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Self-pressurizing rocket propellants are currently gaining popularity in the propulsion community, particularly in hybrid rocket applications. Due to their high vapor pressure, these propellants can be driven out of a storage tank without the need fo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9e8ae35e38e18de12686ebf52fe83047
https://doi.org/10.2514/6.2013-3636
https://doi.org/10.2514/6.2013-3636
Publikováno v:
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Hybrid rockets commonly use nitrous oxide as a self-pressurizing oxidizer, but no comprehensive models exist for predicting the performance of such a system. To aid in the development of such a model, an experimental apparatus has been constructed wi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::16730273668a218da1a2a7d63d98926c
https://doi.org/10.2514/6.2012-4198
https://doi.org/10.2514/6.2012-4198
Publikováno v:
AIAA SPACE 2010 Conference & Exposition.
A hybrid rocket was designed as a demonstrator for the second stage of a Mars Ascent Vehicle for use in a Mars Sample Return mission. Paraffin wax was chosen as the fuel, with liquid nitrous oxide as the oxidizer in order to replicate a Stanford Univ
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1b48bff633874ff94dc53520cf39ff36
https://doi.org/10.2514/6.2010-8840
https://doi.org/10.2514/6.2010-8840