Cold-flow optimization of gaseous oxygen/gaseous hydrogen injectors for the Space Shuttle APS thruster
Gaseous oxygen/gaseous hydrogen auxiliary propulsion engines, considering cold flow experiments with nonreactive simulant gases
Engineering topics
Publications and source records attributed to Nagai, C. K..
Gaseous oxygen/gaseous hydrogen auxiliary propulsion engines, considering cold flow experiments with nonreactive simulant gases
Thermodynamic-kinetic analysis of fluorine/lithium/hydrogen tripropellant combustion efficiency, discussing liquid metal atomization, firings, facility and thrust chamber
Feasibility of lithium-fluorine-hydrogen propellant combination
Rocket performance optimization by extending injector design technology to high performance injectors for space storable FLOX/LPG propellants
Thrust chamber tests on storable liquid rocket propellant
Thermodynamic-kinetic analysis of fluorine/ lithium/hydrogen tripropellant combustion efficiency, discussing liquid metal atomization, firings, facility and thrust chamber
Analysis and design of thrust chamber with gas generator, and thermodynamic-combustion characteristics of lithium-fluorine hydrogen tripropellant combination