Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Aaron D. Olds"'
Autor:
Christopher D. Karlgaard, Paul V. Tartabini, Jay M. Brandon, Roger E. Beck, Stephen D. Derry, Aaron D. Olds, Brett R. Starr
Publikováno v:
Journal of Spacecraft and Rockets. 50:641-661
The Ares I-X trajectory reconstruction produced best-estimated trajectories of the flight-test vehicle ascent through stage separation and of the first- and upper-stage entries after separation. The trajectory-reconstruction process combines onboard,
Publikováno v:
Journal of Spacecraft and Rockets. 44:1060-1070
Global optimization methods have been increasingly under consideration for preliminary interplanetary mission design. One promising global method, differential evolution, has been identified as being particularly well suited to high-thrust trajectory
Autor:
Joseph White, Michael C. Lindell, Ernest L. Bowden, Karl T. Edquist, Aaron D. Olds, F. M. Cheatwood, Brian R. Hollis, David M. Bose, Valerie T. Gsell, Roger E. Beck
Publikováno v:
AIAA Aerodynamic Decelerator Systems (ADS) Conference.
The Inflatable Re-entry Vehicle Experiment 3 (IRVE-3) was conducted from the NASA Wallops Flight Facility on July 23, 2012. Launched on a Black Brant XI sounding rocket, the IRVE-3 research vehicle achieved an apogee of 469 km, deployed and inflated
Autor:
Roger E. Beck, Jay M. Brandon, Christopher D. Karlgaard, Aaron D. Olds, Paul V. Tartabini, Brett R. Starr, Stephen D. Derry
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
The Ares I-X trajectory reconstruction produced best estimated trajectories of the flight test vehicle ascent through stage separation, and of the first and upper stage entries after separation. The trajectory reconstruction process combines on-board
Autor:
F. McNeil Cheatwood, Henry S. Wright, Stephen J. Hughes, Stephen D. Derry, Daniel K. Litton, David M. Bose, Michael C. Lindell, Aaron D. Olds
Publikováno v:
21st AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar.
The suite of Inflatable Re-Entry Vehicle Experiments (IRVE) is designed to further our knowledge and understanding of Hypersonic Inflatable Aerodynamic Decelerators (HIADs). Before infusion into a future mission, three challenges need to be addressed
Publikováno v:
AIAA SPACE 2008 Conference & Exposition.
This paper presents a methodology for performing architecture definition and assessment prior to, or during, program formulation that utilizes a centralized, integrated architecture modeling framework operated by a small, core team of general space a