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 Clapp, S. D..
Gaseous oxygen/gaseous hydrogen auxiliary propulsion engines, considering cold flow experiments with nonreactive simulant gases
Rocket engine propellant injectors with noncircular orifice geometry, presenting experimental spray patterns and predicted performance for noncircular and circular orifice configurations
Thermodynamic-kinetic analysis of fluorine/lithium/hydrogen tripropellant combustion efficiency, discussing liquid metal atomization, firings, facility and thrust chamber
Liquid rocket engine injector elements design criteria, using noncircular orifice geometry to predict efficiency
Reactive stream separation high speed color photography for impinging streams of nitrogen tetroxide and hydrazine
Feasibility of lithium-fluorine-hydrogen propellant combination
Li-F-H tripropellant study, discussing injection method variations and thrust chamber configuration effects on characteristic velocity efficiency and heat flux measurement
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
Analysis, design, and demonstration of high performance injectors for liquid fluorine- gaseous hydrogen propellant combination