Simulation calculations of the Viking qualification flight tests are conducted by use of analytical models of the parachute deployment dynamics process. Results from the study indicate that good simulations of event times and trajectory are obtained. If the full-scale parachute drag coefficient is used, a good simulation of first opening load is obtained and the overall nature of the load history is calculated. For longitudinal motions, the two-degree-of-freedom models give good agreement with a six-degree-of-freedom model. It is believed that the analytical models used are tools which will aid in the analysis of future flight systems
The Advanced Supersonic Parachute Inflation Research Experiments (ASPIRE) project waslaunched to dev...
The work traces a general procedure for the design of a flight simulation tool still representative ...
The deployment characteristics of a 1/8-size dynamically and elastically scaled model of an inflatab...
A six-degree-of-freedom analytical simulation of parachute deployment dynamics developed at the Lang...
Tests of the Viking 16.15-meter nominal-diameter disk-gap-band parachute were conducted at Mach numb...
This report presents the results of Viking Aerothermodynamics Test D4-34.0. Motion picture coverage ...
Flight qualifications for parachutes were tested on full-scale simulated Viking spacecraft at entry ...
The Advanced Supersonic Parachute Inflation Research Experiments (ASPIRE) project waslaunched to dev...
The Crew Exploration Vehicle Parachute Assembly System (CPAS) project is engaged in a multi-year des...
This paper describes an approach to modeling of parachute system’s dynamics inside a synthetic fligh...
The performance of the Viking lander has been evaluated by using a Monte Carlo simulation, and all r...
Models are presented for the aerodynamic coefficients of Supersonic Ringsail and Disk-Gap-Band parac...
Analytical calculations have considered the effects of 1) varying parachute system mass, 2) suspensi...
Four BLDT flights were conducted during the summer of 1972. The purpose of these tests was to qualif...
Balloon Launched Decelerator Test (BLDT) flights were conducted during the summer of 1972 over the W...
The Advanced Supersonic Parachute Inflation Research Experiments (ASPIRE) project waslaunched to dev...
The work traces a general procedure for the design of a flight simulation tool still representative ...
The deployment characteristics of a 1/8-size dynamically and elastically scaled model of an inflatab...
A six-degree-of-freedom analytical simulation of parachute deployment dynamics developed at the Lang...
Tests of the Viking 16.15-meter nominal-diameter disk-gap-band parachute were conducted at Mach numb...
This report presents the results of Viking Aerothermodynamics Test D4-34.0. Motion picture coverage ...
Flight qualifications for parachutes were tested on full-scale simulated Viking spacecraft at entry ...
The Advanced Supersonic Parachute Inflation Research Experiments (ASPIRE) project waslaunched to dev...
The Crew Exploration Vehicle Parachute Assembly System (CPAS) project is engaged in a multi-year des...
This paper describes an approach to modeling of parachute system’s dynamics inside a synthetic fligh...
The performance of the Viking lander has been evaluated by using a Monte Carlo simulation, and all r...
Models are presented for the aerodynamic coefficients of Supersonic Ringsail and Disk-Gap-Band parac...
Analytical calculations have considered the effects of 1) varying parachute system mass, 2) suspensi...
Four BLDT flights were conducted during the summer of 1972. The purpose of these tests was to qualif...
Balloon Launched Decelerator Test (BLDT) flights were conducted during the summer of 1972 over the W...
The Advanced Supersonic Parachute Inflation Research Experiments (ASPIRE) project waslaunched to dev...
The work traces a general procedure for the design of a flight simulation tool still representative ...
The deployment characteristics of a 1/8-size dynamically and elastically scaled model of an inflatab...