Zobrazeno 1 - 10
of 73
pro vyhledávání: '"Arif Karabeyoglu"'
Publikováno v:
Aerospace, Vol 9, Iss 5, p 233 (2022)
Over the past 40 years, the loss rate for commercial passenger aircrafts has decreased down to about one in ten million, whereas the loss rate for spaceflight has remained high, in the 1% range [...]
Externí odkaz:
https://doaj.org/article/460f5e45bcb441d6a39e92b400536226
Publikováno v:
Journal of Propulsion and Power. 38:901-910
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3dc411382e5ec7a8c0179162fea543ff
https://doi.org/10.2514/1.b38681
https://doi.org/10.2514/1.b38681
Publikováno v:
Journal of Propulsion and Power. 38:200-211
Low fuel regression rate is one of the major drawbacks of hybrid rocket motors. In this study, a novel injector concept is proposed to provide a substantial enhancement in the fuel regression rate....
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b3b2a0af21f37f7f567e135ac78a12ab
https://doi.org/10.2514/1.b38417
https://doi.org/10.2514/1.b38417
Publikováno v:
Acta Astronautica. 175:254-267
The objective of this research is to demonstrate the feasibility of sustained combustion in hybrid rocket motor configuration with oxidizers containing high concentrations of C O 2 , an in situ propellant suitable for Mars applications. Motor tests a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4d5cc7e86f76c3e09a25773c48ddcb67
https://doi.org/10.1016/j.actaastro.2020.05.060
https://doi.org/10.1016/j.actaastro.2020.05.060
Autor:
Arif Karabeyoglu, Ozan Kara
This chapter briefly introduces hybrid rocket propulsion for general audience. Advantageous of hybrid rockets over solids and liquids are presented. This chapter also explains how to design a test setup for hybrid motor firings. Hybrid propulsion pro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5fc2fef5e7e063835347e5a256939a31
https://doi.org/10.5772/intechopen.96686
https://doi.org/10.5772/intechopen.96686
Publikováno v:
AIAA Propulsion and Energy 2021 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fe61e24f47ab65e67e62814fd3bbe0ee
https://doi.org/10.2514/6.2021-3507
https://doi.org/10.2514/6.2021-3507
Publikováno v:
AIAA Propulsion and Energy 2021 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5f2ed5e0238319a1d9fa7f0fca2fdbad
https://doi.org/10.2514/6.2021-3248
https://doi.org/10.2514/6.2021-3248
Publikováno v:
AIAA Propulsion and Energy 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::26ad78150d752a94e5f6e302093d59d4
https://doi.org/10.2514/6.2020-3739.c1
https://doi.org/10.2514/6.2020-3739.c1
Publikováno v:
AIAA Propulsion and Energy 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4688b0a6d07e470410a661c36a3e58e5
https://doi.org/10.2514/6.2020-3739
https://doi.org/10.2514/6.2020-3739
Publikováno v:
AIAA Propulsion and Energy 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8fa9de9280299566786ae324e4ebd392
https://doi.org/10.2514/6.2020-3752
https://doi.org/10.2514/6.2020-3752