Zobrazeno 1 - 10
of 16
pro vyhledávání: '"Gregory J. Brauckmann"'
Autor:
Paul M. Danehy, D. P. Patry, Gregory J. Brauckmann, David W. Alderfer, Jennifer A. Inman, S. B. Jones
Publikováno v:
Journal of Spacecraft and Rockets. 46:93-102
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6122e97d0550d11ec60a63078bf9eea8
https://doi.org/10.2514/1.34846
https://doi.org/10.2514/1.34846
Autor:
Brian R. Hollis, Karen T. Berger, Gregory M. Buck, Gregory J. Brauckmann, William A. Wood, Matthew N. Rhode, Thomas J. Horvath, Shann J. Rufer, Scott A. Berry, Derek S. Liechty, Kelly J. Murphy, Michelle L. Mason
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::040a58a00d49b6d19959a2c1f1ebc2fa
https://doi.org/10.2514/6.2015-0213
https://doi.org/10.2514/6.2015-0213
Autor:
F. A. Greene, Richard G. Wilmoth, Gregory J. Brauckmann, Robert A. Mitcheltree, F. M. Cheatwood
Publikováno v:
Journal of Spacecraft and Rockets. 36:429-435
Successful return of interstellar dust and cometary material by the Stardust Sample Return Capsule requires an accurate description of the Earth entry vehicle''s aerodynamics. This desciption must span the hypersonic-rarefied, hypersonic-continuum, s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a125d4332465bbf3fe504ddbf9a8a455
https://doi.org/10.2514/2.3463
https://doi.org/10.2514/2.3463
Publikováno v:
Experiments in Fluids. 26:335-339
A new concept for flow visualization is demonstrated in which fluorescence from locally seeded iodine is viewed in the wake of simple aerodynamic models at Mach 6. Localized seeding is performed by painting a small area of a ceramic model with a tinc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::37cede82461d22781e7f1501578d1b1b
https://doi.org/10.1007/s003480050296
https://doi.org/10.1007/s003480050296
Publikováno v:
Journal of Spacecraft and Rockets. 35:241-248
The effect of isolated roughness on the windward surface boundary layer of the Shuttle Orbiter has been experimentally examined in the NASA Langley Research Center 20-InchMach 6 Tunnel. The size and location of isolated roughness elements (intended t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::433a63295ae7052abf9129b9f08437f3
https://doi.org/10.2514/2.3327
https://doi.org/10.2514/2.3327
Publikováno v:
Journal of Spacecraft and Rockets. 32:758-764
During the high-Mach-number, high-altitude portion of the first entry of the Shuttle Orbiter, the vehicle exhibited a nose-up pitching moment relative to preflight prediction of approximately Delta Cm = 0.03. This trim anomaly has been postulated to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5636d2e82c6ef6cecd27a186119aaeca
https://doi.org/10.2514/3.26680
https://doi.org/10.2514/3.26680
Publikováno v:
29th AIAA Applied Aerodynamics Conference.
The process of developing the nominal static aerodynamic coecients and associated uncertainties for the Orion Crew Module at and below Mach 8 is presented. The database was developed from wind tunnel experiments and computational simulations of the s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::497fbe2aae93c4a71b4d30efa114a9ef
https://doi.org/10.2514/6.2011-3507
https://doi.org/10.2514/6.2011-3507
Autor:
Gregory J. Brauckmann, David T. Chan, Keith B. Paschal, David P. Mayfield, Kelly J. Murphy, Jared Cross, Eric L. Walker, Robert Foley
Publikováno v:
29th AIAA Applied Aerodynamics Conference.
Current Orion Launch Abort Vehicle (LAV) configurations use an eight-jet, solid-fueled Attitude Control Motor (ACM) to provide required vehicle control for all proposed abort trajectories. Due to the forward position of the ACM on the LAV, it is nece
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1234fd84ea400b8cd2565defcfcc7c06
https://doi.org/10.2514/6.2011-3343
https://doi.org/10.2514/6.2011-3343
Autor:
Thomas M. Wilson, Kelly J. Murphy, Matthew N. Rhode, James H. Bell, Gregory J. Brauckmann, David T. Chan, Karen L. Bibb, Bruce Owens, Eric L. Walker
Publikováno v:
29th AIAA Applied Aerodynamics Conference.
The Apollo-derived Orion Crew Exploration Vehicle (CEV), part of NASA s now-cancelled Constellation Program, has become the reference design for the new Multi-Purpose Crew Vehicle (MPCV). The MPCV will serve as the exploration vehicle for all near-te
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::82eb79beb96f2b887786ea2dd1ef3413
https://doi.org/10.2514/6.2011-3502
https://doi.org/10.2514/6.2011-3502
Autor:
Gregory J. Brauckmann, David T. Chan
Publikováno v:
29th AIAA Applied Aerodynamics Conference.
A 6%-scale unpowered model of the Orion Launch Abort Vehicle (LAV) ALAS-11-rev3c configuration was tested in the NASA Langley National Transonic Facility to obtain static aerodynamic data at flight Reynolds numbers. Subsonic and transonic data were o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b949c8f42339be115d9fbc7c4b3a0d22
https://doi.org/10.2514/6.2011-3161
https://doi.org/10.2514/6.2011-3161