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In the Lingard presentation, there is a chart, but it seems upside down. Also cites .5-.55 as a Cd range.
Todo: investigate recently found sources.
Characterize Main
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Determine proper assembly procedures procedures
Review Knacke for gore fullness checks.
Enkles (in Barker with the other parachute books) has some comments.
See Poynter.
Create master list of construction details
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Lingard. 09_Supersonic Parachute Aerodynamic Testing and Fluid Structure Interaction Simulation_Lingard.pdf. (n.d.). Retrieved from https://solarsystem.nasa.gov/docs/09_Supersonic%20Parachute%20Aerodynamic%20Testing%20and%20Fluid%20Structure%20Interaction%20Simulation_Lingard.pdf
Bollermann, B. (1970). A Study of 30 Km to 200 Km Meteorological Rocket Sounding Systems: Literature and data review (2 pts.) (Vol. 1). National Aeronautics and Space Administration.
Clark, I., & Tanner, C. (2017). A historical summary of the design, development, and analysis of the disk-gap-band parachute. In 2017 IEEE Aerospace Conference (pp. 1–17). https://doi.org/10.1109/AERO.2017.7943854
Neal, M., & Wellings, P. (1995). Design and qualification of the descent control sub-system for the Huygens probe. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1533
Maydew, R. C., Peterson, C. W., & Orlik-Rueckemann, K. J. (1991). Design and Testing of High-Performance Parachutes (La Conception et les Essais des Parachutes a Hautes Performances) (No. AGARD-AG-319). ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE), ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE). Retrieved from http://www.dtic.mil/docs/citations/ADA246343
Potvin, J. (2009). Updating and Upgrading the World’s Database on the Opening Shock Factor Ck. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2009-2905
Poynter, D. (1984). The parachute manual: a technical treatise on aerodynamic decelerators (3rd ed., completely rev). Santa Barbara, CA: Para Pub.
Ubico, R. E. (1963). FABRICATION AND DELIVERY OF ARCAS SOUNDING ROCKET SYSTEMS EX 6 MOD 0 AND EX 6 MOD 1. ATLANTIC RESEARCH CORP ALEXANDRIA VA.Neal, M., & Wellings, P. (1995). Design and qualification of the descent control sub-system for the Huygens probe. American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1995-1533