Full-Scale Supersonic Parachute Shape Reconstruction Using Three-Dimensional Stereo Imagery-Reference-Cited by-同舟云学术

Full-Scale Supersonic Parachute Shape Reconstruction Using Three-Dimensional Stereo Imagery

Published:2020-11 Issue:6 Volume:57 Page:1139-1152
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Rabinovitch Jason¹,Griffin Gregory S.¹,Seto William¹,O’Farrell Clara¹,Tanner Christopher L.¹,Clark Ian G.¹

Affiliation:

1. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109

Funder

Jet Propulsion Laboratory

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.A34717

Reference41 articles.

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2. EckstromC. V.PreisserJ. S. “Flight Test of a 30-Foot-Nominal-Diameter Disk-Gap-Band Parachute Deployed at a Mach Number of 1.56 and a Dynamic Pressure of 11.4 Pounds Per Square Foot,” NASA TM X-1451, Aug. 1967.

3. PreisserJ. S.EckstromC. V. “Flight Test of a 40-Foot-Nominal-Diameter Disk-Gap-Band Parachute Deployed at a Mach Number of 1.91 and a Dynamic Pressure of 11.6 Pounds Per Square Foot,” NASA TM X-1575, Aug. 1968.

4. PreisserJ. S.GrowR. B. “High Altitude Flight Test of a Reefed 12.2-Meter Diameter Disk-Gap-Band Parachute With Deployment at a Mach Number of 2.58,” NASA TN D-6469, Aug. 1971.

5. System design overview of the Mars Pathfinder parachute decelerator subsystem

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