Mars Subsonic Parachute Technology Task System Overview-Reference-Cited by-同舟云学术

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Mars Subsonic Parachute Technology Task System Overview

Published:2005-05-23 Issue: Volume: Page:
ISSN:
Container-title:18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar
language:
Short-container-title:

Author:

Witkowski Allen¹,Machalick Walter¹,Taeger Yaor¹

Affiliation:

1. Pioneer Aerospace Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1657

Reference4 articles.

1. High Altitude Test Program for a Mars Subsonic Parachute

2. 2Delurgio,P."EvolutionoftheRingsailParachute,"AIAA-99-1700,1999.

3. 3Ewing,E.G."RingsailParachuteDesign,"AFFDL-TR-72-3,January1972.

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1. Conceptual Common Modular Design for Crew and Cargo Landers and Deep Space Vehicles for Human Exploration of the Solar System;AIAA SPACE 2013 Conference and Exposition;2013-09-10

2. Aerodynamic Characterization of New Parachute Configurations for Low-Density Deceleration;AIAA Aerodynamic Decelerator Systems (ADS) Conference;2013-03-23

3. Design, Development and Verification of the Intermediate eXperimental Vehicle Descent System;21st AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar;2011-05-23

4. Guidance, Navigation, and Control System Performance Trades for Mars Pinpoint Landing;Journal of Spacecraft and Rockets;2010-01

5. Crew and Cargo Landers for Human Exploration of Mars - Vehicle System Design;44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2008-07-21

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