Zobrazeno 1 - 10
of 41
pro vyhledávání: '"F. McNeil Cheatwood"'
Autor:
Christopher A. Kuhl, Jay H. Grinstead, Ashley M. Korzun, Gregory T. Swanson, Brian R. Hollis, Aaron M. Brandis, Karl T. Edquist, Carey Fulton Scott, Scott A. Berry, Jose A. Santos, Christopher D. Karlgaard, Milad Mahzari, Brett A. Cruden, Helen H. Hwang, Cole Kazemba, F. McNeil Cheatwood, Christopher O. Johnston, Mark Schoenenberger, Thomas J. Horvath, Ruth Miller
Publikováno v:
Bulletin of the AAS. 53
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b1f9288ddf9c39cd297bcb493665fe92
https://doi.org/10.3847/25c2cfeb.9045f857
https://doi.org/10.3847/25c2cfeb.9045f857
Publikováno v:
Thin-Walled Structures. 131:869-882
Hypersonic Inflatable Aerodynamic Decelerator (HIAD) systems have the potential to deliver the large payloads required for human-scale Mars missions. The structural response of the HIAD is critical as the inflatable members are relatively compliant c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::04a45e939cd179f01c189c8ab55760ee
https://doi.org/10.1016/j.tws.2018.07.035
https://doi.org/10.1016/j.tws.2018.07.035
Autor:
J. M. DiNonno, John G. Reed, Richard J. Bodkin, Gregory T. Brierly, Stephen J. Hughes, Mohamed M. Ragab, F. McNeil Cheatwood, Allen Lowry, John W. Kelly
Publikováno v:
AIAA SPACE 2016.
For decades, economic reuse of launch vehicles has been an elusive goal. Recent attempts at demonstrating elements of launch vehicle recovery for reuse have invigorated a debate over the merits of different approaches. The parameter most often used t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d47c6002c3cd2e36f824ac070cf652f1
https://doi.org/10.2514/6.2016-5321
https://doi.org/10.2514/6.2016-5321
Autor:
Gregory T. Swanson, Anthony M. Calomino, R. Keith Johnson, Paul Anderson, Brian Gilles, F. McNeil Cheatwood, Stephen J. Hughes, Bruce Bond
Publikováno v:
2016 IEEE Aerospace Conference.
Over a decade of work has been conducted in the development of NASA's Hypersonic Inflatable Aerodynamic Decelerator (HIAD) deployable aeroshell technology. This effort has included multiple ground test campaigns and flight tests culminating in the HI
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d83f79cae8ed69d1bcdf6d1f41d6f537
https://doi.org/10.1109/aero.2016.7500773
https://doi.org/10.1109/aero.2016.7500773
Autor:
Mohamed M. Ragab, F. McNeil Cheatwood
Publikováno v:
AIAA SPACE 2015 Conference and Exposition.
This paper briefly reviews the history of Reusable Launch Vehicle development and recommended reuse techniques based on the lessons learned from those efforts. The paper considers a range of techniques for recovery and reuse of launch vehicles. Launc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0785b7bf363b9e9077183dd4b431c2fe
https://doi.org/10.2514/6.2015-4490
https://doi.org/10.2514/6.2015-4490
Experimental Hypersonic Aerodynamic Characteristics of Mars Surveyor 2001 Precision Lander with Flap
Autor:
Stephen J. Alter, Ramadas K. Prabhu, Tod F. O'Connell, Thomas J. Horvath, F. McNeil Cheatwood
Publikováno v:
Journal of Spacecraft and Rockets. 43:270-281
Aerodynamic wind-tunnel screening tests were conducted on a 0.029-scale model of a proposed Mars Surveyor 2001 Precision Lander (70-deg half-angle spherically blunted cone with a conical afterbody). The primary experimental objective was to determine
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0faeaad91fd6cd1443bcea23e5d8f2d0
https://doi.org/10.2514/1.19651
https://doi.org/10.2514/1.19651
Publikováno v:
The Journal of the Astronautical Sciences. 50:17-33
In the coming decades, several missions will attempt to return samples to Earth from varying parts of the solar system. These samples will provide invaluable insight into the conditions present during the early formation of the solar system, and poss
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d38c05b6d6d2bd15bf1070d57b742be1
https://doi.org/10.1007/bf03546328
https://doi.org/10.1007/bf03546328
Autor:
F. McNeil Cheatwood, Prasun N. Desai
Publikováno v:
Journal of Spacecraft and Rockets. 38:345-350
Genesis will be the first mission to return samples from beyond the Earth-Moon system. The spacecraft will be inserted into a halo orbit about the L1 (Sun-Earth) libration point where it will remain for two years collecting solar wind particles. Upon
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::416a715abd9065b7c67ce01a16c4e830
https://doi.org/10.2514/2.3707
https://doi.org/10.2514/2.3707
Publikováno v:
Journal of Spacecraft and Rockets. 36:421-428
An analysis of the aerothermodynamics and trajectory dispersions experienced by the Mars Polar Lander entry system was performed and is documented herein. Because the Mars Polar Lander aeroshell (forebody) is based on the Mars Path nder aeroshell,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d2a369564827c4f069384337968b7c36
https://doi.org/10.2514/2.3462
https://doi.org/10.2514/2.3462
Publikováno v:
Journal of Spacecraft and Rockets. 36:412-420
The Mars Microprobe mission will provide the e rst opportunity for subsurface measurements, including water detection, near the Mars south pole. Performance of the Microprobe aeroshell design is evaluated through development and application of a six-
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d7ec455f16ff0c49cbed68c3f458a381
https://doi.org/10.2514/2.3461
https://doi.org/10.2514/2.3461