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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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Static longitudinal stability and control characteristics of air-to-surface canard missile configuration in transonic range
Free flight test of tailless missile configuration with 45-deg sweptback wing of aspect ratio 4 - stability at transonic speeds
Application of photoelasticity in missile industry - stress analysis of propellant grains
Space science - telemetry for guided missiles and space vehicle carrier systems - from v2 to saturn
Human error in reliability testing of missile systems
Simultaneous missile launching - statistical analysis
Statistical analysis of missile launching
Wind tunnel tests of wingless low aspect ratio folding control missile configurations
Materials-research areas of importance to missile and spacecraft structure
Measurement, description and presentation of wind data for missile and space vehicle design
Pressure distribution on base and afterbody of missile configuration with and without jet flow using single and multiple nozzles
Wind profiles and missile and spacecraft design
Mathematical model of missile launching
Static longitudinal stability and control characteristics of wingless missile configuration at supersonic and hypersonic speeds
Static longitudinal stability and control characteristics of hypersonic missile configuration with all movable cruciform wing and tail surfaces
Wind tunnel tests - effect of wind induced loads on dynamically scaled model of large missile in launching position
Derivation of set of linearized dynamic equations for use in missile stability analyses