Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Mike Loucks"'
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 50:877-888
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e7448c15bddde023af09fd2c1ff081f5
https://doi.org/10.5139/jksas.2022.50.12.877
https://doi.org/10.5139/jksas.2022.50.12.877
Autor:
Doug Sinclair, Jonathan Currie, Richard Hunter, Mike Loucks, Richard G. French, Ehson Mosleh, Peter Beck
Publikováno v:
Bulletin of the AAS. 53
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b1ecca4b9f2c2cd542eb6af466c877db
https://doi.org/10.3847/25c2cfeb.8b85beed
https://doi.org/10.3847/25c2cfeb.8b85beed
Publikováno v:
Icarus. 347:113792
For any asteroid on an impact trajectory, the amount of time prior to impact a deflection can be implemented can drastically change the amount of deflection impulse required. In this study we use the precision cloud-based asteroid orbit propagation a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::79e3cb7ec5bc6592c900b0fe0a93ad28
https://doi.org/10.1016/j.icarus.2020.113792
https://doi.org/10.1016/j.icarus.2020.113792
Autor:
Daniel J. Rasky, John Carrico, Allison F. Zuniga, Daniel Policastri, Mark Turner, Mike Loucks
Publikováno v:
AIAA SPACE and Astronautics Forum and Exposition.
A new concept study was initiated to examine the architecture needed to gradually develop an economical, evolvable and sustainable lunar infrastructure using a public/private partnerships approach. This approach would establish partnership agreements
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f547c3e38f9d9c61f28f8fd82331472f
https://doi.org/10.2514/6.2017-5148
https://doi.org/10.2514/6.2017-5148
Publikováno v:
AIAA SPACE and Astronautics Forum and Exposition.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::35ead1bf0e6163ea0403317ef443ba1c
https://doi.org/10.2514/6.2017-5148.c1
https://doi.org/10.2514/6.2017-5148.c1
Autor:
Peter J. Edelman, Mike Loucks, John Carrico, Dennis A. Tito, Kyle M. Hughes, James M. Longuski
Publikováno v:
AIAA/AAS Astrodynamics Specialist Conference.
All Mars free-return trajectories to Earth are found over this century, which are comparable to the Inspiration Mars mission. Trajectories are found emphasizing the desirable characteristics of a short total time-of-flight (TOF), low launch energy, a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a069eb5dbd97f071a9fe66056ee70ac1
https://doi.org/10.2514/6.2014-4128
https://doi.org/10.2514/6.2014-4128
Autor:
Peter J. Edelman, Mike Loucks, Dennis A. Tito, Kyle M. Hughes, John Carrico, James M. Longuski
Publikováno v:
AIAA/AAS Astrodynamics Specialist Conference.
Mars free-return trajectories that use a Venus flyby either before or after the Mars encounter are found, and an alternative launch opportunity for the Inspiration Mars mission is identified. Launch dates are searched from 2015 to 2060, and focus is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::11703f993ae9b2737983e7f98502a24b
https://doi.org/10.2514/6.2014-4109
https://doi.org/10.2514/6.2014-4109
Autor:
Lisa Policastri, David J. McComas, M. Reno, Nathan A. Schwadron, Ryan Lebois, B. Hautamaki, Mark B. Tapley, John Carrico, M. Intelisano, Mike Loucks, R. Tyler, John Scherrer
Publikováno v:
Space Weather. 9
[1] NASA's Interstellar Boundary Explorer (IBEX) mission was recently maneuvered into a unique long-term stable Earth orbit, with apogee at ∼50 Earth radii (RE). The Moon's (∼65 RE) gravity disrupts most highly elliptical Earth orbits, leading to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::70e97e5d51a5d4d0909d293d0029662e
https://doi.org/10.1029/2011sw000704
https://doi.org/10.1029/2011sw000704
Publikováno v:
AIAA/AAS Astrodynamics Specialist Conference.
This paper describes the orbit covariance analysis performed before and during IBEX operations to ensure that mission requirements are met. The authors describe how they calculated the orbit covariance during different mission phases, from launch thr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f73d267e26fac87677ca560c1c178b44
https://doi.org/10.2514/6.2010-7981
https://doi.org/10.2514/6.2010-7981
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