Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Christine E. Szalai"'
Autor:
Robin Beck, Jarvis T. Songer, Mark A. Johnson, David Saunders, Christopher D. Karlgaard, Christine E. Szalai
Publikováno v:
Journal of Spacecraft and Rockets. 58:1582-1589
The Mars Interior Exploration using Seismic Investigations, Geodesy and Heat Transport (InSight) spacecraft, which successfully touched down on the planet surface on November 26, 2018, was proposed...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cfcad3ac8c0c1adeb0a9ed448a5415bc
https://doi.org/10.2514/1.a35078
https://doi.org/10.2514/1.a35078
Publikováno v:
Journal of Spacecraft and Rockets. 51:1167-1173
The Mars Science Laboratory is a scientific mission that placed a 900 kg rover with 10 science instruments on the surface of Mars. A key component for landing on the surface of Mars is the aeroshell, which decelerates the entry vehicle to just 1% of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::263df73299bc2ce4410599e8be3ac963
https://doi.org/10.2514/1.a32673
https://doi.org/10.2514/1.a32673
Mars Exploration Rover Transverse Impulse Rocket Cover Thermal Protection System Design Verification
Publikováno v:
Journal of Spacecraft and Rockets. 42:990-998
Arc jet test results are summarized of the Mars Exploration Rover silicone-impregnated reusable ceramic ablator (SIRCA) transverse impulse rocket system (TIRS) cover test series in the Panel Test Facility at NASA Ames Research Center. The primary obj
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::75ab5be04175a3acef1050de6a28737c
https://doi.org/10.2514/1.3637
https://doi.org/10.2514/1.3637
Autor:
Huy K. Tran, Kelly E. Parmenter, Christine E. Szalai, Daniel J. Rasky, Frederick Milstein, Karl Shuman
Publikováno v:
Journal of Spacecraft and Rockets. 39:290-298
Silicone impregnated reusable ceramic ablators are highly porous fibrous ceramic substrates that are partially impregnated with silicone. The ablators are used as heat shields for planetary entry. The compressive responses of virgin and charred ablat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::102c3e814b11d5f55e56ecf09655613d
https://doi.org/10.2514/2.3811
https://doi.org/10.2514/2.3811
Autor:
Huy K. Tran, Frederick Milstein, Christine E. Szalai, Daniel J. Rasky, Karl Shuman, Kelly E. Parmenter
Publikováno v:
Journal of Spacecraft and Rockets. 38:231-236
Lightweight ceramic ablators are porouse brousceramicsubstrates impregnated with organicresins. Thematerialsweredevelopedforuseasheatshieldsforplanetaryentry.Thecompressiveresponseandhardnessofaphenolic impregnated carbon ablator and its e brous subs
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e7bb1663e4107896f83dc78cb1867a1f
https://doi.org/10.2514/2.3675
https://doi.org/10.2514/2.3675
Publikováno v:
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
With the gradual increase in robotic rover sophistication and the desire for humans to explore the solar system, the need for reentry systems to deliver large payloads into planetary atmospheres is looming. Heritage ablative Thermal Protection System
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::58702a521e5814d1133dfa4365118b3c
https://doi.org/10.2514/6.2012-472
https://doi.org/10.2514/6.2012-472
Autor:
Ethiraj Venkatapathy, Benjamin L. Thoma, William H. Willcockson, Todd White, Wayne J. Lee, Justin N. Maki, Christine E. Szalai
Publikováno v:
42nd AIAA Thermophysics Conference.
For the first time ever, engineers were able to observe a heatshield on the surface of another planet after a successful entry through the atmosphere. A three-week heatshield observation campaign was conducted in December 2004 after the Mars Explorat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b6cdeab29271c4523facc26344f8f309
https://doi.org/10.2514/6.2011-3956
https://doi.org/10.2514/6.2011-3956
Autor:
Matthew Gasch, Christine E. Szalai, Jeffrey G. Gragg, Antonella I. Alumni, Jose F. Chavez-Garcia, Amy Brewer, Scott C. Splinter, Robin Beck
Publikováno v:
42nd AIAA Thermophysics Conference.
The Entry, Descent, and Landing (EDL) Technology Development Project has been tasked to develop Thermal Protection System (TPS) materials for insertion into future Mars Entry Systems. A screening arc jet test of seven rigid ablative TPS material cand
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::33a6b322851733564c4abc834ca0664b
https://doi.org/10.2514/6.2011-3493
https://doi.org/10.2514/6.2011-3493
Publikováno v:
2011 Aerospace Conference.
Mars Science Laboratory is a scientific mission that places a 900 kg rover with 10 science instruments on the surface of Mars. 12A key component for landing on the surface of Mars is the aeroshell, which decelerates the entry vehicle to just 1% of it
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b044853e5ac95a954835dea883a30bd5
https://doi.org/10.1109/aero.2011.5747500
https://doi.org/10.1109/aero.2011.5747500