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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Two-stage test turbine for operation in high temperature saturated potassium vapor - fluid dynamic testing, mechanical design and testing, facility modifications, and turbine testing
Ultralight honeycomb development for Saturn S-II STAGE improvement - titanium bonding, core sandwich construction, and testing
Performance characteristics of repetitively pulsed two-stage plasma propulsion engine
Manufacturing checkout of orbital operational Saturn S-IVB stage and instrument unit for parking orbit operations
Manufacture, assembly, and static tests of Saturn S-IB-1 stage
Performance testing of two-stage potassium vapor turbines
Parametric performance of two-stage repetitively pulsed plasma engine
Two-stage potassium turbine endurance testing and performance characteristics
Mechanical design of two-stage impulse turbine for liquid hydrogen turbopump of M-1 engine
Connector development, selection, and inspection for Saturn S-IV stage propulsion system
Efficiency evaluation of two-stage turbine with low ratio of blade to jet speed suitable for bleed-type high energy liquid rocket applications
Transonic aerodynamic characteristics of two-stage fin-stabilized rocket launch vehicle in combination with winged spacecraft
Proof pressure, functional, dielectric, humidity, temperature, vibration, life cycle, and impact tests for qualifying Saturn S-IB stage LOX REPLENISHING ball valve
Reliability design concepts in cryogenic fluid systems in Saturn S-IV stage propulsion system, noting hydrogen and LOX tank pressurization systems
Optimal steering and staging of multistage boosters using extended variational method to include variable discontinuities at corners
Base heating in Saturn S-IV stage from exhaust reversal, comparing flight and scale model data
Welding of aluminum alloy for S-1C stage of Saturn-Apollo space vehicle
Contractor components/parts reliability program for Douglas S-IVB stage project