Zobrazeno 1 - 10
of 30
pro vyhledávání: '"Marlow D. Moser"'
Publikováno v:
Journal of Propulsion and Power. 23:175-180
The low regression rates of classic hybrid rocket fuels lead to large internal ports that limit potential applications. This experimental study investigated the increase in regression rate that results from adding a solid oxidizer and a catalyst to a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2ea463e6a31c1b3483a700ee85484dfc
https://doi.org/10.2514/1.14327
https://doi.org/10.2514/1.14327
Publikováno v:
51st AIAA/SAE/ASEE Joint Propulsion Conference.
The work presented here is a study of a digital method for determining the combustion bomb burning rate of a fuel-rich gas generator propellant sample using the ultrasonic pulse-echo technique. The advanced digital method, which places user defined l
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dff9d429495d96732b77683342bff4a2
https://doi.org/10.2514/6.2015-4103
https://doi.org/10.2514/6.2015-4103
Publikováno v:
Journal of Heat Transfer. 126:155-160
Vacuum insulation panels have values of thermal conductivity that are extremely low ∼4mW/ms˙K compared to the thermal conductivity of most common insulations. Typical ASTM test methods are not designed for testing these very low thermal conductivi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a3830ef222f89cbe3608bcb0cf7fac43
https://doi.org/10.1115/1.1683674
https://doi.org/10.1115/1.1683674
Publikováno v:
Review of Scientific Instruments. 70:4416-4421
This article illustrates the application of an ultrasonic pulse–echo technique to determine the burning rate of a composite solid propellant as a function of pressure. An evaluation of the measurement uncertainty of the method is also presented. Un
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6bc153f8c128c21fd9c47e158fd29213
https://doi.org/10.1063/1.1150087
https://doi.org/10.1063/1.1150087
Publikováno v:
Journal of Propulsion and Power. 15:155-158
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::82697f183dea0c60e5d42e6c06c339db
https://doi.org/10.2514/2.5406
https://doi.org/10.2514/2.5406
Publikováno v:
Journal of Propulsion and Power. 19:713-715
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::09799420e7ab0eaf47b4988b56c69aa5
https://doi.org/10.2514/2.6161
https://doi.org/10.2514/2.6161
Publikováno v:
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
The goal of Charger Rocket Works (CRW) is to design, build and fly a reusable rocket carrying a scientific payload. This is part of a National Aeronautics and Space Administration (NASA) sponsored competition for universities around the nation to com
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b8e6992a6d71bc5913568cc3b3a2a1f6
https://doi.org/10.2514/6.2010-6935
https://doi.org/10.2514/6.2010-6935
Publikováno v:
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
A geometrically full-scale swirl injector element was subjected to cold flow testing to explore the influence of steady chamber pressure on spray characteristics and selfatomization at conditions that reflect real liquid rocket combustor conditions.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4aac0a0e54b25f12a8e4512551183f17
https://doi.org/10.2514/6.2010-6665
https://doi.org/10.2514/6.2010-6665
Autor:
David M. Lineberry, Marlow D. Moser, Robert L. Ikard, M. S. Balasubramanyam, Robert A. Frederick
Publikováno v:
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::07f2dc27f01bfe555756297f2904ffc1
https://doi.org/10.2514/6.2010-6737
https://doi.org/10.2514/6.2010-6737
Publikováno v:
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
The Propulsion Research Center has developed a liquid oxygen propellant feed system which has advanced into the next stage of operational maturity. As part of the design review process, an oxygen compatibility and hazards assessment was developed and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4e3578049deeb898b39fa1f2852ae9cb
https://doi.org/10.2514/6.2010-6810
https://doi.org/10.2514/6.2010-6810