Don't have Adobe Acrobat Reader?
Download it for free here! |
 |
|
|
The use of LS-DYNA to Assess the Performance of Airborne Systems
North Americaís Candidate ATPS Main Parachutes
Presented at the AIAA Aerodynamic Decelerator Systems
Technology Conference and Published by AIAA, May 2005,
Munich, Germany |
|
The use of LS-DYNA to Simulate the Inflation of a Parachute
Canopy
Presented at the AIAA Aerodynamic Decelerator Systems
Technology Conference and Published by AIAA, May 2005, Munich, Germany |
|
The DCLDYN Parachute Inflation and Trajectory Analysis Tool
Presented at the AIAA Aerodynamic Decelerator Systems
Technology Conference and Published by AIAA, May
2005, Munich, Germany |
|
Floatstab A Tool for the Rapid Analysis of Flotation Stability
Presented at the AIAA Aerodynamic Decelerator Systems
Technology Conference and Published by AIAA,
May 2005, Munich, Germany |
|
|
An
Investigation of the Apparent Mass of Parachutes under Post Inflation
Dynamic Loading using FSI Simulation
Presented at the AIAA Aerodynamic Decelerator Systems
Technology Conference and Published by AIAA, May 2003, Monterey,
California |
|
|
An
Overview of the Landing System for the K-1 Launch Vehicle Parachutes
and Airbags
Presented at the AIAA Aerodynamic Decelerator Systems Technology
Conference and Published by AIAA, June 1997, San Francisco, California |
|
|
Application
of Optimization Software to Aid the Design of an Airbag Decelerator
System
Presented at the AIAA Aerodynamic Decelerator Systems Technology
Conference and Published by AIAA, May 2003, Monterey, California |
|
|
Atmospheric
Reentry Demonstrator Parachute Recovery Assembly
Presented at the AIAA Aerodynamic Decelerator Systems Technology
Conference and Published by AIAA, June 1997, San Francisco, California |
|
|
Design
and Development of the Main Parachute for the Beagle 2 Mars Lander
Presented at the AIAA Aerodynamic Decelerator Systems Technology Conference
and Published by AIAA, May 2003, Monterey, California |
|
|
Design
and Testing of an Airbag Landing Attenuator System for a Generic Crew
Return Vehicle
Presented at the AIAA Aerodynamic Decelerator Systems Technology Conference
and Published by AIAA, May 2005, Munich, Germany |
|
|
Design
and Testing of the HOPE-X HSFD-II Landing System
Presented at the AIAA Aerodynamic Decelerator Systems Technology Conference
and Published by AIAA, May 2001, Boston, Massachusetts |
|
|
Design
and Testing of the K1 Reusable Launch Vehicle Landing System Airbags
Presented at the AIAA Aerodynamic Decelerator Systems Technology Conference
and Published by AIAA, June 1999, Toulouse, France |
|
|
Recovery
System for the Evolved Expendable Launch Vehicle
Presented at the AIAA Aerodynamic Decelerator Systems Technology Conference
and Published by AIAA, June 1997, San Francisco, California |
|
|
The
Application of Explicit Finite Element Analysis and Fluid Structure
Interaction Simulations for Recovery Systems
Presented at the 41st SAFE Symposium, September 2003, Jacksonville,
Florida |
|
|
The
System Approach to Spin Stall Parachute Recovery Systems A Five Year
Update
Presented at the Society of Experimental Test Pilots Symposium, September
2004, Los Angeles, California |
|
|
The
use of LS-DYNA to Simulate the Airbag Landing Impact Attenuation of
the Kistler K1 Reusable Launch Vehicle
Presented at the 5th International LS-DYNA Userís Conference,
September 1998, Detroit, Michigan |
|
|
The
use of LS-DYNA to Simulate the Water Landing Characteristics of Space
Vehicles
Presented at the 8th International LS-DYNA Userís Conference,
May 2004, Detroit, Michigan |
|
|
Recovery
Systems Design Guide AFFDL-TR-78-151
This
handbook is a comprehensive guide to the practicing engineer in
the field of recovery system design, construction and testing.
This
handbook was prepared by Irvin Industries Inc, California Division
under Air Force Contract Number F33615-75-C-3081. The principal
authors were Mr. E.G.Ewing, Mr. H.W.Bixby and Mr. T.W.Knacke.
NOTE:
This is a large file, may take some time to download.
|