Zobrazeno 1 - 10
of 31
pro vyhledávání: '"Paul V. Tartabini"'
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,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::142262efaedc5515c423c1f242ffb0c4
https://doi.org/10.2514/1.a32345
https://doi.org/10.2514/1.a32345
Autor:
Christopher D. Karlgaard, Mathew D. Toniolo, Carlos M. Roithmayr, Bandu N. Pamadi, Paul V. Tartabini, Jamshid A. Samareh
Publikováno v:
Journal of Spacecraft and Rockets. 50:191-205
A = axial location of the solid rocket booster (SRB) reference point in Space Shuttle main engine (SSME) plume coordinate system, ft ax, ay, az = acceleration components along body axes (excluding components due to gravity), ft=s CA = isolated (frees
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::735af5ee0f20ffe1a8fcbe6e1844971d
https://doi.org/10.2514/1.a32048
https://doi.org/10.2514/1.a32048
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
The NASA Engineering and Safety Center initiated the Max Launch Abort System (MLAS) Project to investigate alternate crew escape system concepts that eliminate the conventional launch escape tower by integrating the escape system into an aerodynamic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ff614f3b8bacaea98c3ffa650b5d110d
https://doi.org/10.2514/6.2016-0783
https://doi.org/10.2514/6.2016-0783
Autor:
Bandu N. Pamadi, Christopher D. Karlgaard, Paul V. Tartabini, Matthew D. Toniolo, Carlos M. Roithmayr
Publikováno v:
Journal of Spacecraft and Rockets. 48:573-583
This paper discusses the application of the constraint force equation methodology and its implementation for multibody separation problems using three specially designed test cases. The first test case involves two rigid bodies connected by a fixed j
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5b17d93ce1bbffee74afd5cad8e6389e
https://doi.org/10.2514/1.51943
https://doi.org/10.2514/1.51943
Autor:
Christopher D. Karlgaard, Paul V. Tartabini, Robert C. Blanchard, Michael Kirsch, Matthew D. Toniolo
Publikováno v:
Journal of Spacecraft and Rockets. 43:105-115
The formulation and development of a trajectory reconstruction tool for the NASA X-43A/Hyper-X high-speed research vehicle and its implementation for the reconstruction and analysis of flight-test data are discussed. Extended Kalman filtering techniq
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f0070523c6c7a861e7a66275a4507698
https://doi.org/10.2514/1.12733
https://doi.org/10.2514/1.12733
Publikováno v:
Journal of Spacecraft and Rockets. 42:423-434
The Mars 2001 Odyssey Orbiter successfully completed the aerobraking phase of its mission on 11 January 2002. The support provided by NASA’s Langley Research Center to the navigation team at the Jet Propulsion Laboratory, California Institute of Te
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ff7824d39918b2fc028e09526947d1cb
https://doi.org/10.2514/1.15175
https://doi.org/10.2514/1.15175
Publikováno v:
Journal of Spacecraft and Rockets. 39:788-795
As part of phase 2 of the X-33 Program, NASA selected an integrated lifting body/aerospike engine configuration as the study vehicle for the conceptual analysis of a single-stage-to-orbit reusable launch vehicle. A team at NASA Langley Research Cente
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f04c89887cb1c359b04eeac488538f86
https://doi.org/10.2514/2.3880
https://doi.org/10.2514/2.3880
Publikováno v:
The Journal of the Astronautical Sciences. 50:191-211
Atmospheric density data taken during the Mars Global Surveyor aerobraking mission (1997-1999) showed significant variability over the altitude ranges (100-140 km) of interest for aerobraking. This paper presents the method by which Mars Global Surve
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0b4ff567a9cda1d8743cf7e879507fff
https://doi.org/10.1007/bf03546262
https://doi.org/10.1007/bf03546262
Publikováno v:
Journal of Spacecraft and Rockets. 34:334-340
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c3da83059bc03a0a7916bde6a291806e
https://doi.org/10.2514/2.3213
https://doi.org/10.2514/2.3213
Autor:
Prasun N. Desai, Paul V. Tartabini
Publikováno v:
Journal of Spacecraft and Rockets. 32:250-256
This study determines the effect on the initial mass in low Earth orbit (IMLEO) of delaying departure from Mars and Earth by 5, 15, and 30 days, once a nominal mission to Mars has been selected. Additionally, the use of a deep-space maneuver (DSM) is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::def4029b9bed5eba08923bc10ef9e8ea
https://doi.org/10.2514/3.26603
https://doi.org/10.2514/3.26603