Some test results from the NASA planetary entry parachute program.
NASA planetary entry parachute program for rocket launched and balloon deployment tests
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NASA planetary entry parachute program for rocket launched and balloon deployment tests
Mission sequential environment effects on Dacron parachute material mechanical properties
Equations of motion for parachute deployment analysis
Performance test on disk gap band parachute at supersonic speeds
Development and testing of planetary landing parachute system
Testing Dacron parachute components and assemblies by exposure to ethylene oxide sterilization, simulated package loading, and heat cycle
High altitude flight test of ringsail parachute with deployment at Mach 2.95
Design of parachutes and ballutes for decelerating atmospheric entries at supersonic velocities
Test program for determining visual reference requirements for pilot control of gliding parachutes used in landing spacecraft on land
Fireball effect on launch abort parachute heating of manned spacecraft
Design and performance of ringsail parachute
Multiple parachute system for landing control of Apollo type spacecraft
Parachute system for lowering manned spacecraft from post-reentry to ocean landing
Opening distance and inflation time prediction for parachutes deployed supersonically based on subsonic performance
Parachute altitude wind sensor /PAWS/ project for real time wind profile determination, using modified HASP I sounding rocket
Mission sequential environment effects on Dacron parachute material mechanical properties
Spacecraft parachute stress analysis, using finite elements with nonlinear elastic properties to obtain shape and load distribution
Parachute canopy surfaces transient aerodynamic pressures during unsteady processes, using piston theory