Investigation of the starting characteristics of the M-1 rocket engine using the analog computer
Starting characteristics of M- I liquid propellant rocket engine using analog computer simulation
ANALOG SIMULATION↗
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Aerodynamic Design and Estimated Performance of a Two-stage Curtis Turbine for the Liquid Oxygen Turbopump of the M-1 Engine
Two-stage turbine for liquid oxygen turbopump of M-1 rocket engine
LIQUID OXYGEN /LOX/↗
Hydraulic design of the M-1 liquid hydrogen turbopump
Hydraulic design of axial flow hydrogen turbopump for M-1 rocket engine
TURBOPUMP↗
Summary of observed results when chilling the M-1 fuel turbopump to liquid hydrogen temperature
Cooling tests of M-1 rocket engine turbopump with liquid hydrogen
TURBOPUMP↗
Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine. II - Overall two-stage performance
Cold flow test of pump drive turbines for M-1 rocket engine
M-1 ROCKET ENGINE↗
Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine. I - Inlet feedpipe-manifold assembly
Cold air performance of scale model oxidizer pump drive turbine feedpipe-manifold-nozzle assembly for M-1 rocket engine
COLD FLOW TEST↗
M-1 engine test complex data acquisition systems
Instrumentation and data acquisition system for development testing of liquid hydrogen/liquid oxygen M-1 rocket engine
ENGINE TESTING↗
Large size cryogenic turbine type flowmeter technology
Procurement, calibration, installation, and use of cryogenic turbine flowmeters for M-1 engine
TURBINE ENGINE↗
Cooled baffle development for M-1 engine using a subscale rocket engine
Film and transpiration cooled baffles for M-1 engine
Conrad, E. W.↗
Summary of materials technology of M-1 engine
Mechanical and physical properties of materials used in M-1 liquid hydrogen/liquid oxygen rocket engine
PHYSICAL PROPERTY↗
The mechanical design of a two-stage impulse turbine for the liquid hydrogen turbopump of the M-1 engine
Mechanical design of two-stage impulse turbine for liquid hydrogen turbopump of M-1 engine
M-1 ROCKET ENGINE↗
Mechanical design of a Curtis turbine for the oxidizer turbopump of the M-1 engine
Turbine mechanical design for M-1 engine oxidizer turbopump
M-1 ROCKET ENGINE↗
Development of LO2/LH2 Gas Generators for the M-1 Engine
Liquid oxygen/liquid hydrogen gas generator development for M-1 engine
GAS GENERATOR↗
Cooldown of large-diameter liquid hydrogen and liquid oxygen lines
Cooldown of large-diameter liquid hydrogen and liquid oxygen propellant piping systems at M-1 engine test complex
CRYOGENIC PROPELLANT↗
Economic analysis of Perlite versus super insulation in liquid hydrogen storage and run vessels for the M-1 Program
Cost comparison of perlite and multilayer aluminum foil relective insulation in liquid hydrogen storage dewars for M-1 engine
THERMAL INSULATION↗
Development of liquid oxygen cooled 110MM ROLLER and tandem ball bearings at up to .5 x 106 DN values for the oxidizer turbopump of the M-1 engine Technology report
Bearing package design suitability for M-1 liquid oxygen turbopump
M-1 ROCKET ENGINE↗
Fabrication of lightweight turbine components using electron-beam welding for the attachment of sheet metal blades to discs and shrouds
Fabrication of lightweight turbine components for M-1 engine oxidizer turbopump using electron beam welding for attaching sheet metal blades to discs and shrouds
TURBOPUMP↗
Design and development of liquid hydrogen cooled 120mm roller, 110mm roller, and 110mm tandem ball bearings for M-1 fuel turbopump
Liquid hydrogen cooled tandem ball bearings for M-1 fuel turbopump
M-1 ROCKET ENGINE↗