Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Mark D. Klem"'
Autor:
Hiroshi Ueno, Eric A. Hurlbert, Hiroya Asakawa, Jean-Marc Ruault, Chiara Manfletti, Leslie Alexander, Ryan Whitley, Wesley L. Johnson, Mark D. Klem, Emanuela D'Aversa, Jean-Noel Caruana
As part of the Global Exploration Roadmap (GER), the International Space Exploration Coordination Group (ISECG) formed two technology gap assessment teams to evaluate topic discipline areas that had not been worked at an international level to date.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::de9311406a83bde1c413eba693a4a395
https://elib.dlr.de/110759/
https://elib.dlr.de/110759/
Publikováno v:
AIAA SPACE 2010 Conference & Exposition.
The Propulsion and Cryogenics Advanced Development (PCAD) Project s primary objective is to develop propulsion system technologies for nontoxic or "green" propellants. The PCAD project focuses on the development of nontoxic propulsion technologies ne
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::718d28307135f43ad156df2d99e75794
https://doi.org/10.2514/6.2010-8680
https://doi.org/10.2514/6.2010-8680
Autor:
James E. Giuliani, Mark D. Klem
Publikováno v:
28th Joint Propulsion Conference and Exhibit.
The ROCket Combustor Interactive Design (ROCCID) methodology is an interactive computer program that combines previously developed combustion analysis models to calculate the combustion performance and stability of liquid rocket engines. Test data fr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ddcbe634e3cb220e1c6366a8d6e62b7d
https://doi.org/10.2514/6.1992-3226
https://doi.org/10.2514/6.1992-3226
Autor:
Kevin J. Breisacher, Mark D. Klem
Publikováno v:
26th Joint Propulsion Conference.
Test data from NASA Lewis' Effect of Thrust Per Element on Combustion Stability Characteristics of Hydrogen-Oxygen Rocket Engines test program are used to validate two recently released stability analysis tools. The first tool is a design methodology
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3275d6590bf79532886e2844f9de2ceb
https://doi.org/10.2514/6.1990-2241
https://doi.org/10.2514/6.1990-2241
Publikováno v:
26th Joint Propulsion Conference.
The ROCket Combustor Interactive Design (ROCCID) Methodology is a newly developed, interactive computer code for the design and analysis of a liquid propellant rocket combustion chamber. The application of ROCCID to design a liquid rocket combustion
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::75eee71680d420e00135c4fb5b283626
https://doi.org/10.2514/6.1990-2240
https://doi.org/10.2514/6.1990-2240