Controlled deceleration specimen protection systems for electrodynamic vibration systems
Controlled deceleration specimen protection systems for electrodynamic vibration systems
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Controlled deceleration specimen protection systems for electrodynamic vibration systems
Shallow water tow channel used to study two dimensional compressible wake of supersonic decelerator
Drag characteristics of toroid-membrane and wide-angle conical shells used as towed decelerators
Deployment and steady state performance of supersonic attached inflatable decelerator canopy models
Bluff-shaped annular configuration for supersonic decelerator for reentry vehicles
Entry and terminal deceleration systems for unmanned Martian landers, discussing parachute landing and lifting entry vehicles
Parachute design for decelerating upper atmosphere rocket probes at high altitudes, using high drag coefficients in Stokes flow regime
VTOL flight investigation to develop decelerating instrument approach capability with control- command information display for three degrees of freedom
Initial deceleration of solar wind positive ions upstream of earth bow shock determined from OGO 5 high time resolution plasma measurements
Parachute decelerator towline energy absorber shock attenuation characteristics, discussing drop test results
Decelerator fabric elastic constants for structural analyses using generalized Hookes law
Nonuniform free stream supersonic flow past aerodynamic decelerators, calculating inviscid flow fields by method of characteristics
Snatch force during lines-first deployment of aerodynamic decelerator, including effects of canopy skirt acceleration and suspension wave propagation characteristics
Attached Inflatable Decelerator for planetary atmospheric entry, discussing mission applications and wind tunnel models performance
Parachute decelerator system for 1975 Viking Mars Lander mission, discussing configuration selection, design factors, trajectory simulation, weight and mass analysis, etc
Development and characteristics of hot air balloon deceleration and recovery system
VTOL display and control system for deceleration to instrument hover
Design, fabrication and static testing of attached inflatable decelerator models for supersonic wind tunnel evaluation