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Green Liquid Monopropellant ThrusterPhysical Sciences, Inc. (PSI), and Orbital Technologies Corporation (ORBITEC) are developing a unique chemical propulsion system for next-generation NASA science spacecraft and missions. The system is compact, lightweight, and can operate with high reliability over extended periods of time and under a wide range of thermal environments. The system uses a new storable, low-toxicity liquid monopropellant as its working fluid. In Phase I, the team demonstrated experimentally the critical ignition and combustion processes for the propellant and used the data to develop thruster design concepts. In Phase II, the team developed and demonstrated in the laboratory a proof-of-concept prototype thruster. A Phase III project is envisioned to develop a full-scale protoflight propulsion system applicable to a class of NASA missions.
Document ID
20160005352
Acquisition Source
Glenn Research Center
Document Type
Other
Authors
Joshi, Prakash B.
(Physical Sciences, Inc. Andover, MA, United States)
Date Acquired
April 26, 2016
Publication Date
July 1, 2015
Publication Information
Publication: An Overview of SBIR Phase 2 In-Space Propulsion and Cryogenic Fluids Management
Subject Category
Propellants And Fuels
Spacecraft Propulsion And Power
Engineering (General)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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