Evaluation of entry and terminal deceleration systems for unmanned Martian landers
Entry and terminal deceleration systems for unmanned Martian landers, discussing parachute landing and lifting entry vehicles
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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
Trajectory, thermodynamic, and stress analyses of spacecraft inflatable decelerators in Mars and Earth atmospheres
Design, fabrication, and static testing of wind tunnel models of first-stage Attached Inflatable Decelerator canopies for supersonic vehicles
Adhesive and coating material formulations and manufacturing processes for lightweight low-permeability braces for use in high altitude decelerators
Mach 8 variable-density tunnel used for determination of aerodynamic heating of attached inflatable decelerator configurations
Deceleration of low energy cosmic rays in solar wind involving Fermi acceleration by MHD waves and adiabatic energy change