System design overview of the Mars Pathfinder parachute decelerator subsystem

Author:

Fallon, II Edward1,Fallon, II Edward1

Affiliation:

1. Pioneer Aerospace Corp., South Windsor, CT

Publisher

American Institute of Aeronautics and Astronautics

Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Full-Scale Supersonic Parachute Shape Reconstruction Using Three-Dimensional Stereo Imagery;Journal of Spacecraft and Rockets;2020-11

2. ASPIRE Aerodynamic Models and Flight Performance;AIAA Aviation 2019 Forum;2019-06-15

3. Summary of the Advanced Supersonic Parachute Inflation Research Experiments (ASPIRE) Sounding Rocket Tests with a Disk-Gap-Band Parachute;AIAA Aviation 2019 Forum;2019-06-14

4. Entry, Descent and Landing Systems;The International Handbook of Space Technology;2014

5. Design and Development of the Main Parachute for the Beagle 2 Mars Lander;17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar;2003-05-19

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