Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Shruti Dipak Jadhav"'
Publikováno v:
4. 1:1-6
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9ca8c06016adf8f99496dfb216bf98c8
https://doi.org/10.46632/jame/1/4/1
https://doi.org/10.46632/jame/1/4/1
Publikováno v:
3. 1:29-38
Experimental sounding rockets are important contributors to aerospace engineering research. However, experimental-sounding rockets are rarely used for student research projects by institutes in India. The unavailability of rocket motors, which requir
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::19dd2db7ac4644e06cb7d8a70c174526
https://doi.org/10.46632/jame/1/3/5
https://doi.org/10.46632/jame/1/3/5
Autor:
null Shruti Dipak Jadhav, null Raghvendra Pratap Singh, null Atri Bandyopadhyay, null Tapas Kumar Nag
Publikováno v:
international journal of engineering technology and management sciences. 6:368-373
In the era of cryogenic propellants with high specific impulse; under microgravity situations, long-term storage and higher energy thruster management are highly needed. As methane is a reasonable cooling membrane for radiation and ablation chambers
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::de14d3e1d4594ac63ec4df06ceb46d0a
https://doi.org/10.46647/ijetms.2022.v06i06.065
https://doi.org/10.46647/ijetms.2022.v06i06.065
Publikováno v:
Graduate Research in Engineering and Technology. :45-48
The solid rocket motor upper stage for a space launch vehicle is a more efficient propulsion technology than the liquid rocket motor upper stage. Its grain design has the potential to be crucial in terms of lowering inert mass by adopting improved vo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dc6d4cc879832dc8bf0d5bec15552e57
https://doi.org/10.47893/gret.2022.1105
https://doi.org/10.47893/gret.2022.1105
Publikováno v:
1. 8:48-51
Hybridrocket motors are widely used in heavy launch vehicles with maximum payload capacity. The main reason for the study in this field is that the hybrid rocket motor is very easy to handle and has a simple design. In this paper, we have studied the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6f45acd88d08d83b19d02180c328da0f
https://doi.org/10.46632/jemm/8/1/9
https://doi.org/10.46632/jemm/8/1/9
Publikováno v:
Graduate Research in Engineering and Technology. :133-139
Blended wing body is a fixed wing aircraft which are smoothly blended together with no clear dividing line and no distinct wings also be given a wide Aerofoil shaped body. The future transportation is of aircrafts will incline towards the aerodynamic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::10c059c792e564dc3479ebd191a5436e
https://doi.org/10.47893/gret.2022.1046
https://doi.org/10.47893/gret.2022.1046