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An Overview of In-Space Propulsion and Cryogenics Fluids Management Efforts for 2014 SBIR Phases I and IINASA's Small Business Innovation Research (SBIR) program focuses on technological innovation by investing in the development of innovative concepts and technologies to help NASA's mission directorates address critical research and development needs for Agency programs. This report highlights 11 of the innovative SBIR 2014 Phase I and II projects from 2010 to 2012 that focus on one of NASA Glenn Research Center's six core competencies-In-Space Propulsion and Cryogenic Fluids Management. The technologies cover a wide spectrum of applications such as divergent field annular ion engines, miniature nontoxic nitrous oxide-propane propulsion, noncatalytic ignition systems for high-performance advanced monopropellant thrusters, nontoxic storable liquid propulsion, and superconducting electric boost pumps for nuclear thermal propulsion. Each article describes an innovation and technical objective and highlights NASA commercial and industrial applications. This report provides an opportunity for NASA engineers, researchers, and program managers to learn how NASA SBIR technologies could help their programs and projects, and lead to collaborations and partnerships between the small SBIR companies and NASA that would benefit both.
Document ID
20160012396
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Nguyen, Hung D.
(NASA Glenn Research Center Cleveland, OH United States)
Steele, Gynelle C.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
October 18, 2016
Publication Date
October 1, 2016
Subject Category
Spacecraft Propulsion And Power
Propellants And Fuels
Report/Patent Number
GRC-E-DAA-TN27289
NASA/TM-2016-219153
E-19275
Funding Number(s)
WBS: WBS 471296.01.03.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
divergent field annular ion engine
nuclear thermal propulsion
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