Zobrazeno 1 - 10
of 21
pro vyhledávání: '"Christopher L. Tanner"'
Autor:
Christopher L. Tanner, William Seto, Jason Rabinovitch, Clara O'Farrell, Ian G. Clark, G. S. Griffin
Publikováno v:
Journal of Spacecraft and Rockets. 57:1139-1152
This paper describes three-dimensional (3D) stereo reconstruction efforts for the full-scale supersonic parachute deployment tests performed under the NASA Advanced Supersonic Parachute Inflation R...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aa8e97eb60ae0344b545f650624d61ea
https://doi.org/10.2514/1.a34717
https://doi.org/10.2514/1.a34717
Publikováno v:
AIAA Aviation 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b2bf7300eaf423fcb03cafc2f9e2ef6b
https://doi.org/10.2514/6.2019-3479
https://doi.org/10.2514/6.2019-3479
Autor:
William Seto, Ian G. Clark, Jason Rabinovitch, Clara O'Farrell, Christopher L. Tanner, G. S. Griffin
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dfe49c23fcabd3f77b30f19936e4de1f
https://doi.org/10.2514/6.2019-1629
https://doi.org/10.2514/6.2019-1629
Publikováno v:
2018 Atmospheric Flight Mechanics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a58fc5c445bc002370522899222d1bb4
https://doi.org/10.2514/6.2018-3623
https://doi.org/10.2514/6.2018-3623
Publikováno v:
2018 IEEE Aerospace Conference.
In 2012, the Mars Science Laboratory (MSL) landed safely on the surface of Mars using a supersonic Disk-Gap-Band (DGB) parachute, which was structurally qualified for flight via a subsonic wind tunnel test program. Results of the Low-Density Superson
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::259ff08c75574222314efdfb4976ae1d
https://doi.org/10.1109/aero.2018.8396717
https://doi.org/10.1109/aero.2018.8396717
Autor:
Christopher L. Tanner, Ian G. Clark
Publikováno v:
2017 IEEE Aerospace Conference.
The Disk-Gap-Band (DGB) parachute was originally developed in the late 1960's by Clint Eckstrom for high-altitude meteorological rocket applications. It was designed as a balance between drag and stability with a relatively simplistic design and low
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5d1f80f37ee9e629009ece34903cbd7d
https://doi.org/10.1109/aero.2017.7943854
https://doi.org/10.1109/aero.2017.7943854
Autor:
Suman Muppidi, John C. Gallon, Christopher L. Tanner, Clara O'Farrell, Erich Brandeau, Ian G. Clark
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
NASA’s Low-Density Supersonic Decelerators project (LDSD) has developed and tested four new aerodynamic decelerator technologies for future Mars missions: two attached toroidal inflatable decelerators, a ballute, and a large supersonic parachute. O
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::88458770847368605b3e7b4b9bc89846
https://doi.org/10.2514/6.2016-3242
https://doi.org/10.2514/6.2016-3242
Publikováno v:
2016 IEEE Aerospace Conference.
Mars landers are mass limited by the available entry, descent, and landing technology. The Mars Science Laboratory rover pushed the boundaries of EDL technology to land 900 kg of rover at an elevation of −4.5 km MOLA (Mars Orbiter Laser Altimeter)
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2c055741360aeb083c37a25f7ebbb0f0
https://doi.org/10.1109/aero.2016.7500790
https://doi.org/10.1109/aero.2016.7500790
Publikováno v:
Journal of Spacecraft and Rockets. 46:340-352
The 2009 Mars science laboratory mission is being designed to place an 850 kg rover on the surface of Mars at an altitude of at least one kilometer. This is being accomplished using the largest aeroshell and supersonic parachute ever flown on a Mars
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1abe0880be5913509186b9caddfd1510
https://doi.org/10.2514/1.38562
https://doi.org/10.2514/1.38562
Autor:
Christopher L. Tanner, Clara O'Farrell, John C. Gallon, Ian G. Clark, Deepak Bose, Allen Witkowski, Paul J. Woodruff
Publikováno v:
23rd AIAA Aerodynamic Decelerator Systems Technology Conference.
The Low Density Supersonic Decelerator (LDSD) Project required the use of a pilot system due to the inability to mortar deploy its main supersonic parachute. A mortar deployed 4.4 m diameter supersonic ram-air ballute was selected as the pilot system
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f3fac6e677b0fb77a0a0a0d3d812fba7
https://doi.org/10.2514/6.2015-2128
https://doi.org/10.2514/6.2015-2128