Experimental and analytical comparison of flowfields in a 110 N (25 lbf) H2/O2 rocket [PDF]
A gaseous hydrogen/gaseous oxygen 110 N (25 lbf) rocket was examined through the RPLUS code using the full Navier-Stokes equations with finite rate chemistry. Performance tests were conducted on the rocket in an altitude test facility.
Kim, Suk C. +3 more
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Experimental evaluation of resistojet thruster plume shields [PDF]
The exhaust of an engineering model resistojet has been investigated using rotary pitot probes and a rotary quartz crystal microbalance. The resistojet operated on CO2 propellant at a mass flow rate of 0.29 g/sec in both heated and unheated flows ...
Bailey, Allan B., Carney, Lynnette M.
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The Green Propellant Infusion Mission Thruster Performance Testing for Plume Diagnostics [PDF]
The Green Propellant Infusion Mission (GPIM) is sponsored by NASA's Space Technology Mission Directorate (STMD) Technology Demonstration Mission (TDM) office.
Arrington, Lynn A. +6 more
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Green Propellant Infusion Mission Program Development and Technology Maturation [PDF]
The NASA Space Technology Mission Directorate's (STMD) Green Propellant Infusion Mission (GPIM) Technology Demonstration Mission (TDM) is comprised of a cross-cutting team of domestic spacecraft propulsion and storable green propellant technology experts.
Aggarwal, Pravin K. +10 more
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Development of an analytical model of hydrazine decomposition motors [PDF]
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Crespo Martínez, Antonio +4 more
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An Overview of In-Space Propulsion and Cryogenics Fluids Management Efforts for 2014 SBIR Phases I and II [PDF]
NASA'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 ...
Nguyen, Hung D., Steele, Gynelle C.
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A Flexible Lunar Architecture for Exploration (FLARE) supporting NASA's Artemis Program. [PDF]
Acta Astronaut, 2020 Evans ME, Graham LD.
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Green Liquid Monopropellant Thruster [PDF]
Physical Sciences, Inc. (PSI), and Orbital Technologies Corporation (ORBITEC) are developing a unique chemical propulsion system for next-generation NASA science spacecraft and missions.
Joshi, Prakash B.
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Development and design of a 10 N monopropellant thruster.
Transactions of the Institute of Aviation, 2015 Samantha Booth +3 more
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An Overview of SBIR Phase 2 In-Space Propulsion and Cryogenic Fluids Management [PDF]
Technological innovation is the overall focus of NASA's Small Business Innovation Research (SBIR) program. The program invests in the development of innovative concepts and technologies to help NASA's mission directorates address critical research and ...
Nguyen, Hung D., Steele, Gynelle C.
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