Aerodynamic Characterization of New Parachute Configurations for Low-Density Deceleration-Reference-Cited by-同舟云学术

Aerodynamic Characterization of New Parachute Configurations for Low-Density Deceleration

Published:2013-03-23 Issue: Volume: Page:
ISSN:
Container-title:AIAA Aerodynamic Decelerator Systems (ADS) Conference
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Author:

Tanner Christopher L.¹,Clark Ian G.¹,Gallon John¹,Rivellini Tommaso¹,Witkowski Allen²

Affiliation:

1. Jet Propulsion Laboratory, California Institute of Technology

2. Pioneer Aerospace Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1358

Reference15 articles.

1. 1McBride, D. D. “Orbiter Drag Chute Stability Test in the NASA Ames 80x120 Foot Wind Tunnel,” Tech. Rep. SAND93-2544, Sandia National Laboratories, Albuquerque, NM, Feb. 1994.

2. Mars Subsonic Parachute Technology Task System Overview

3. High Altitude Test Program for a Mars Subsonic Parachute

4. Low Density Supersonic Decelerator Parachute Decelerator System

5. Wind Tunnel Testing of Various Disk-Gap-Band Parachutes

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