Diode Laser Absorption Spectroscopy Measurements in a Gaseous Hydrogen / Oxygen Rocket

Locke, Justin M.; Pal, Snehanshu; Woodward, Roger; Santoro, Robert J.

doi:10.2514/6.2011-688

Cited by 4 publications

(1 citation statement)

References 44 publications

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“…. 6,7,8 The third area is Multi-Physics Modeling. This included scales from the combustion of individual ammonium perchlorate particles, unit physics simulations , 9,10,11. all the way up to modeling the performance of a complex system in one simulation.…”

Section: Introductionmentioning

confidence: 99%

Strategies for Successful University, Industry, and Government Collaborations

Frederick¹

2014

50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference

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Advances in rocket propulsion technology have historically relied on a healthy interaction among members of the university, industry, and government communities. The National Institute of Rocket Propulsion Systems commissioned a series of three Academic Workshops from 2011 to 2014 to gather information about the current status of research at universities and recommend strategies for successful collaborations. This paper summarizes the activities of these workshops. A snapshot of propulsion research at universities is summarized from Workshop I. Workshop II produced a series of health metrics by which one could monitor the well-being of university propulsion programs and a description of how individual universities organized their efforts. In Workshop III, representatives of the university, industry, and government examined three case studies on larger university-based activities, which interacted heavily with government and involved industry. Participants assessed desirable attributes such as continuity of support, sustainability, industry mentorship, multi-disciplinary collaboration, and shared curricula. University coalitions that operate under non-profit research and graduate education institute appear to be an excellent strategy for current and future sustainable university, government, and industry programs in rocket propulsion systems.

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Section: Introductionmentioning

confidence: 99%