System scheme design for LOX/LCH4 variable thrust liquid rocket engines using motor pump
The Status of the Research and Development of LNG Rocket Engines in Japan
On porous liquid propellant rocket engine injectors
Analysis and experimental verification of axial thrust on the M-1 liquid oxygen turbopump
Analysis and Experimental Verification of Axial Thrust on the M-1 Liquid Oxygen Turbopump
Design and Development Status of Experimental Winged Rocket WIRES#015
Effect of Liquid Nitrogen Dilution on LOX Impact Sensitivity
A Preliminary Investigation of Oxidizer-Rich Oxygen-Hydrogen Combustion Characteristics
Analysis of Fluorine Addition to the Vanguard First Stage
Development of LO2/LH2 Gas Generators for the M-1 Engine