Design and economic aspects of reusable launch vehicles and considerations for future systems
Engineering feasibility and economics of reusable launch vehicle systems
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Engineering feasibility and economics of reusable launch vehicle systems
Stopped and stowed rotor V/STOL transport aircraft designs, discussing results of full scale wind tunnel tests of start-stop process
Entropy relations identity proved between two dimensional functions related by Fourier transformation, noting spacecraft communication implications
Lift drag ratios attainable by slender bodies at hypersonic speeds assuming modified Newtonian pressure distribution and surface constant friction coefficient
Apollo antenna design before and after reentry, discussing radio blackout problems and S band helices performance
Sliding contact problems in tilting pad gas bearings at high temperatures, considering material selection
Centrifugal slinger seal dynamic and thermal design and performance properties determined by laminar flow analysis
Spacecraft utilization for earth resources noting remote sensing programs in meteorology, geodesy, oceanography, hydrology and geology
Equivalent noise circuit applicable to active RF feedback amplifier
Centrifugal slinger seal dynamic and thermal design and performance properties determined by laminar flow analysis
Small scientific satellite design guidelines and concepts, noting flexibility regarding accommodation of variety of missions for magnetosphere studies
Radioisotope electrogenerators based on beta emitting fuels, discussing design and aerospace applications
Thin metal films deposition on substrates, discussing nucleation and growth
Quality and reliability control of spacecraft toroidal transformers noting material selection, termination techniques, performance testing, etc
Airplane design analysis by operational similarity parameters and coefficients, noting aircraft applications range from DC-3 to SST
Etiology of neonatal mortality in rats bred and raised at 3,800 meters from low-land parents
Theory and clearance effects on stability of water lubricated herringbone-groove journal bearings
Trajectory analysis for mission to Jupiter in 1972