Zobrazeno 1 - 10
of 33
pro vyhledávání: '"Ashley C. Karp"'
Autor:
Brian J. Cantwell, David Dyrda, Ashley C. Karp, Jason Rabinovitch, Flora S. Mechentel, Elizabeth T. Jens
Publikováno v:
Journal of Propulsion and Power. 36:773-782
The performance of a diode laser igniter as a restart-capable device has been assessed for single-port, poly(methyl methacrylate) (PMMA)/gaseous oxygen (GOX) hybrid motors. For this testing a proto...
Publikováno v:
Journal of Propulsion and Power. 36:33-46
This work was undertaken in an effort to improve the understanding of the combustion processes inside classical and fast-burning hybrid rocket motors. In this paper, a combustion visualization expe...
Autor:
George Whittinghill, Greg Zilliac, George Story, Brian J. Evans, Barry Nakazono, Ashley C. Karp
Publikováno v:
AIAA Propulsion and Energy 2020 Forum.
Publikováno v:
AIAA Propulsion and Energy 2020 Forum.
Autor:
Jason Rabinovitch, David Dyrda, Elizabeth T. Jens, Ashley C. Karp, Barry Nakazono, Flora S. Mechentel, Kyle T. Williams
Publikováno v:
AIAA Propulsion and Energy 2019 Forum.
Autor:
Elizabeth T. Jens, Flora S. Mechentel, Brian J. Cantwell, David Dyrda, Ashley C. Karp, Jason Rabinovitch
Publikováno v:
AIAA Propulsion and Energy 2019 Forum.
Autor:
Andrew S. Prince, Timothy P. Kibbey, Andrew Schnell, Darius Yaghoubi, Ashley C. Karp, Barry Nakazono
Publikováno v:
AIAA Propulsion and Energy 2019 Forum.
A solid propulsion system design is being considered for a conceptual Mars Ascent Vehicle (MAV) as part of a potential robotic Mars Sample Return campaign. A Preliminary Architecture Assessment for a MAV is being conducted at Marshall Space Flight Ce
Autor:
Darius Yaghoubi, Gregory G. Zilliac, Ashley C. Karp, Andrew Schnell, Barry Nakazono, George Story
Publikováno v:
AIAA Propulsion and Energy 2019 Forum.
Autor:
Ashley C. Karp, Brian K. Muirhead
Publikováno v:
2019 IEEE Aerospace Conference.
This paper will provide an overview of current concepts and options for the architecture and design of a Mars Sample Return Lander (called Sample Return Lander, SRL). Key mission objectives and the overall baseline mission design will be described, i