Design of Subscale Parachute Models for MSL Supersonic Wind Tunnel Testing-Reference-Cited by-同舟云学术

Design of Subscale Parachute Models for MSL Supersonic Wind Tunnel Testing

Published:2009-05-04 Issue: Volume: Page:
ISSN:
Container-title:20th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar
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Short-container-title:

Author:

Witkowski Allen¹,Kandis Mike¹,Reuter James¹,Machalick Walter¹,Kelsch Richard²,Sengupta Anita³

Affiliation:

1. Pioneer Aerospace Corp.

2. NASA Glenn Research Center

3. California Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-2999

Reference25 articles.

1. Acanopy material of low-permeability was a specification requirement in order to simulate the effective permeability of parachute fabric operating in the low density Martian atmosphere. A standard 1.17 oz/yd2parachute fabric having a porosity range of 0.5 to 5.0 ft3/ft2/min under 0.5 in H2O pressure differential, PIA-C-44378C, was selected. select ConfluenceBridleand RiserExtension Construction

2. PN11673 32.00 804.2 2.56* 2.64*** 5.15 5.47 24 0.07 7.5 0.268 0.226 1.700 1.767 1.926 1.993 3.221 3.481 0.00401

3. plug PN11708 32.00 804.2 3.30* 3.42*** 8.55 9.19 24 0.12 7.5 1.000 3.142 1.728 2.386 4.870 5.528 3.173 3.660 0.00401

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