Zobrazeno 1 - 10
of 16
pro vyhledávání: '"Scott A. Striepe"'
Autor:
Rafael Lugo, Richard W. Powell, John M. Carson, Scott A. Striepe, Christopher D. Karlgaard, Alicia M. Dwyer-Cianciolo, Jake A. Tynis, Ronald R. Sostaric, David Woffinden
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a8452f4a3dd03329db9c114bda9d7e78
https://doi.org/10.2514/6.2019-0661
https://doi.org/10.2514/6.2019-0661
Publikováno v:
Journal of Spacecraft and Rockets. 43:311-323
Two primary simulations have been developed and are being updated for the Mars Science Laboratory entry, descent, and landing. The high-fidelity engineering end-to-end entry, descent, and landing simulation is based on NASA Langley Research Center's
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d1ee5f47da98151ff7f0f6067793e8b9
https://doi.org/10.2514/1.19649
https://doi.org/10.2514/1.19649
Flight data from an entry, descent, and landing sequence can be used to reconstruct the vehicle's trajectory, aerodynamic coefficients, and the atmospheric profile experienced by the vehicle. Past Mars missions have not contained instrumentation that
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a8b1aecdbe59eda8f4fa533400fce080
https://resolver.caltech.edu/CaltechAUTHORS:20230310-764772000.28
https://resolver.caltech.edu/CaltechAUTHORS:20230310-764772000.28
Autor:
Richard W. Powell, Bruce Jackson, Curtis Zimmerman, Jeremy D. Shidner, Albert Jackson, Michael J. Weinstein, Scott Reardon, Deleena M. Noble, Eric M. Queen, Scott A. Striepe, Robert Shelton, Michael M. Madden, Manuel P. Castro, Emily K. Lewis, Daniel K. Litton, William I. Sellers, Nghia D. Vuong, John Aguirre
Publikováno v:
AIAA Modeling and Simulation Technologies (MST) Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8e273285717a5d2517560d09a1e273f8
https://doi.org/10.2514/6.2013-5071
https://doi.org/10.2514/6.2013-5071
Publikováno v:
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Flight data from an entry, descent, and landing (EDL) sequence can be used to reconstruct the vehicle's trajectory, aerodynamic coefficients and the atmospheric profile experienced by the vehicle. Past Mars missions have contained instruments that do
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d6e70e108d68957fb3ecd7d551558b91
https://doi.org/10.2514/6.2012-400
https://doi.org/10.2514/6.2012-400
Publikováno v:
Journal of Spacecraft and Rockets. 31:543-549
Mars trajectory design options were examined that would accommodate a premature termination of a nominal manned opposition class mission for opportunities between 2010 and 2025. A successful abort must provide a safe return to Earth in the shortest p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::407e21320cc65ac2ed110c4aa3ccbef3
https://doi.org/10.2514/3.26476
https://doi.org/10.2514/3.26476
Publikováno v:
Journal of Spacecraft and Rockets. 30:420-425
Many current manned Mars mission studies are using low lift-to-drag ratio vehicles to aerobrake at both Mars and Earth. This paper will demonstrate that if entry velocity constraints are incorporated into the interplanetary analysis of aerobraking Ma
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2ab8b20418c2653345506049e7b741b1
https://doi.org/10.2514/3.25547
https://doi.org/10.2514/3.25547
Publikováno v:
Journal of Spacecraft and Rockets. 30:426-430
Many current manned Mars mission studies are using low lift-to-drag ratio (L/D) vehicles to aerobrake at both Mars and Earth. The use of these low L/D vehicles could limit the allowable velocity at the atmospheric interface. This paper will demonstra
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e697e9730e41c6c183fdb393306e0943
https://doi.org/10.2514/3.25548
https://doi.org/10.2514/3.25548
Publikováno v:
Journal of Spacecraft and Rockets. 29:801-807
The human radiation environment for several short-duration stay manned Mars missions is predicted using the Mission Radiation Calculation (MIRACAL) program, which was developed at NASA Langley Research Center. This program provides dose estimates for
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::407c13db6acf46332c22edb953e4ace5
https://doi.org/10.2514/3.25534
https://doi.org/10.2514/3.25534
Autor:
Brian R. Hollis, Naruhisa Takashima, Scott A. Striepe, Deepak Bose, Michael J. Wright, Kenneth Sutton
Publikováno v:
38th AIAA Thermophysics Conference.
An investigation of the aerothermodynamic environment of the Huygens entry probe has been conducted. A Monte Carlo simulation of the trajectory of the probe during entry into Titan's atmosphere was performed to identify a worst-case heating rate traj
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2e45a494a84be31a8be6719e22d1f05c
https://doi.org/10.2514/6.2005-4816
https://doi.org/10.2514/6.2005-4816