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pro vyhledávání: '"Catherine Mollmann"'
Autor:
Jared Daum, Catherine Mollmann
Publikováno v:
24th AIAA Aerodynamic Decelerator Systems Technology Conference.
Autor:
Catherine Mollmann
Publikováno v:
24th AIAA Aerodynamic Decelerator Systems Technology Conference.
Throughout their lifecycle, parachute textiles come into contact with various other substances. This contact may occur during manufacturing and repair, storage and transportation, packing, or actual use. While this interaction does not always result
Autor:
Catherine Mollmann
Publikováno v:
24th AIAA Aerodynamic Decelerator Systems Technology Conference.
A parachute joint is defined as a location where a component is sewn or connected to another component. During the design and developmental phase of a parachute system, the joints for each structural component are isolated and tested through a proces
Autor:
Brian P. Anderson, Patrick W. Goulding, Laura K. Kushner, James S. Greathouse, Barry J. Porter, Edward T. Schairer, James C. Ross, Jessica M. Powell, Catherine Mollmann, Matthew L. Zwicker
Publikováno v:
24th AIAA Aerodynamic Decelerator Systems Technology Conference.
A two-week test campaign was conducted in the National Full-Scale Aerodynamics Complex 80 x 120-ft Wind Tunnel in support of Orion parachute pendulum mitigation activities. The test gathered static aerodynamic data using an instrumented, 3-tether sys
Autor:
Catherine Mollmann
Publikováno v:
24th AIAA Aerodynamic Decelerator Systems Technology Conference.
During the developmental testing program for CPAS (Capsule Parachute Assembly System), the parachute system for the NASA Orion Crew Module, simulation revealed that high loads may be experienced by the pilot risers during the most devere deployment c
Autor:
Catherine Mollmann
Publikováno v:
23rd AIAA Aerodynamic Decelerator Systems Technology Conference.
This paper details the methodology for determining the joint factor for all parachute components. This method has been successfully implemented on the Capsule Parachute Assembly System (CPAS) for the NASA Orion crew module for use in determining the