David E A Reichenau

发表

AERODYNAMIC PERFORMANCE OF VARIOUS HYPERFLO AND HEMISFLO PARACHUTES AT MACH NUMBERS FROM 1.8 TO 3.0

David E A Reichenau, 1965 .

Aerodynamic Characteristics of Disk-Gap-Band Parachutes in the Wake of Viking Entry Forebodies at Mach Numbers from 0.2 to 2.6

David E A Reichenau, 1972 .

INVESTIGATION OF VARIOUS FULL-SCALE PARACHUTES AT MACH NUMBER 3.0

David E A Reichenau, 1965 .

INVESTIGATION OF AN ATTACHED INFLATABLE DECELERATOR SYSTEM FOR DRAG AUGMENTATION OF THE VOYAGER ENTRY CAPSULE AT SUPERSONIC SPEEDS

David E A Reichenau, 1968 .

Deployment and Performance Characteristics of Attached Inflatable Decelerators with Mechanically Deployed Inlets at Mach Numbers from 2.6 to 4.5

David E A Reichenau, 1972 .

Aerodynamic Characteristics of an Ejection Seat Escape System with Cold Flow Rocket Plume Simulation at Mach Numbers from 0.6 through 1.5.

David E A Reichenau, 1969 .