Zobrazeno 1 - 10
of 34
pro vyhledávání: '"Boris Yendler"'
Autor:
Boris Yendler, Steven H. Collicott
Publikováno v:
Journal of Spacecraft and Rockets. 59:482-488
Dangers of assuming symmetric liquid and gas positioning in symmetric tanks with symmetric propellant management device vanes are identified. Examples from spaceflight history plus modeling of prop...
Autor:
Boris Yendler
The role of the thermal control system is to keep temperature of the components within required temperature limits for given orbits, power demand, operations, etc. It also should reduce temperature gradients across the spacecraft and some components
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::06b2eefbe8dc7d2824f382535ee9efe9
https://doi.org/10.1016/b978-0-12-817884-3.00016-3
https://doi.org/10.1016/b978-0-12-817884-3.00016-3
Autor:
Kira Abercromby, Fernando Aguado Agelet, José Miguel Lago Agra, Krisjani Angkasa, Alessandra Babuscia, James Barrington-Brown, Simone Battistini, Jacob Beningo, Chantal Cappelletti, Mengu Cho, James W. Cutler, Pedro Luiz Kaled Da Cás, Nathan D. Fite, David C. Folta, Arno Formella, Anthony Freeman, Jose L. Garcia, Alessandro Golkar, Filippo Graziani, Kyle Hughs, Santiago Iglesias Cofán, Shigeru Imai, Danil Ivanov, Andrew T. Klesh, Mary Knapp, Naomi Kurahara, Benjamin K. Malphrus, Alberto González Muíño, Yuichiro Nogawa, Chris Ostrom, Mikhail Ovchinnikov, Khary I. Parker, Antonio J. Ricco, Daniel Robson, Sergio R. Santa Maria, Robert Staehle, Sergey Trofimov, Ricardo Tubío-Pardavila, Joost Vanreusel, Andrés Eduardo Villa, Roger Walker, Boris Yendler, Luis Zea
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6305ba75f05fb1855ed48a99bb4a91e8
https://doi.org/10.1016/b978-0-12-817884-3.09992-6
https://doi.org/10.1016/b978-0-12-817884-3.09992-6
Autor:
Boris Yendler, Steven H. Collicott
Publikováno v:
AIAA Propulsion and Energy 2019 Forum.
Publikováno v:
SpaceOps 2016 Conference.
Publikováno v:
Journal of Spacecraft and Rockets. 44:878-883
An unbalanced propellant load in a geosynchronous communications satellite with multiple tanks can reduce satellite life. Depending on the details of the propellant plumbing system, significant fuelmay become unusable in the more full tanks when the
Publikováno v:
SpaceOps 2014 Conference.
Publikováno v:
AIAA SPACE 2013 Conference and Exposition.
Publikováno v:
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
A successful mission planning, in particular, at End-of-Life (EOL) depends on many factors including an accurate knowledge of remaining propellant, as a one of the major factors. Achieving the highest accuracy of propellant estimation is very importa
Autor:
Boris Yendler
Publikováno v:
AIAA SPACE 2012 Conference & Exposition.
There are a lot of stories about spacecraft rescue. The majority of them describe efforts by engineers or operators in qualitative terms without looking at the technology which facilitates the spacecraft rescue. This paper discusses real cases and di