Some fracture considerations in the design and analysis of spacecraft pressure vessels.
Probable failure mode and minimum service life prediction for spacecraft pressure vessels using fracture mechanics analysis and fracture specimen test results
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Probable failure mode and minimum service life prediction for spacecraft pressure vessels using fracture mechanics analysis and fracture specimen test results
CdS solar cell model, discussing p-n junction, CdS and copper sulfide properties and microscopic junction formation and behavior
Comparative evaluation of interference factor corrections in wind tunnel tests on vertical takeoff aircraft models
Preliminary design concept of jet lift research aircraft reaction control system
Time division access system for satellite communications, and figure of merit for effects of bit and frequency synchronization
Moon to earth return trajectory analysis
Lunar module backup guidance, navigation and pilot interfaces with control systems during lunar landing missions
Size and shield weight requirements calculated for fast-spectrum, liquid-metal cooled nuclear reactor for space power application
Approximate average midspan metal temperatures and coolant flow requirements for turbine airfoils cooled by compressor exit bleed air
Meteorological and geodetic satellite networks for earth resources survey
Human psychological engineering factors in development and implementation of display media
Single versus multiple engine configurations for Voyager capsule bus propulsion
High voltage design specifications for detector assembly /ultraviolet photon counters/ used in Goddard experimental package
Fitzgerald-Hallpike caloric test of vestibular function
Systems analysis and performance of deep space communication equipment, and tracking and navigation studies on Earth-Mars flyby mission
Characteristics of liquid metal cooled reactor gaseous fission products vented or contained, for space power systems
Cycle characteristics and structural configuration of turbojet and turbofan engines for lightweight aircraft
Eigen-vibration representation of transfer functions for structures by considering arbitrary excitations