Development and Testing of an 8m Isotensoid Supersonic Inflatable Aerodynamic Decelerator (SIAD)-Reference-Cited by-同舟云学术

Development and Testing of an 8m Isotensoid Supersonic Inflatable Aerodynamic Decelerator (SIAD)

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

Author:

Coatta Daniel¹,Jurewicz David A.²,Tutt Benjamin A.²,Clark Ian G.¹,Rivellini Tommaso¹

Affiliation:

1. Jet Propulsion Laboratory, California Institute of Technology

2. Airborne Systems

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1328

Reference14 articles.

1. Some test results from the NASA planetary entry parachute program.

2. Optimization of inflatable drag devices by isotensoid design

3. 4Bohon, H. L., and Miserentino, R. "Deployment and Performance Characteristics of 5-Foot-Diameter Attached Inflatable Decelerators fromMach Number 2.2to4.4," NASA TN D-5840,1970.

4. 5Bohon, H. L., Sawyer, J. W., and Miserentino, R. "Deployment and Performance Characteristics of 1.5-Meter Supersonic Attached Inflatable Decelerators," NASA TN D-7550,1974.

Cited by 9 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. On the History and Semantics of Burble in Aerodynamic Theory;AIAA SCITECH 2024 Forum;2024-01-04

2. Computational Analysis and Post-Flight Validation of Ballute Aerodynamics;23rd AIAA Aerodynamic Decelerator Systems Technology Conference;2015-03-27

3. Stress Analysis of the LDSD Supersonic Ballute;23rd AIAA Aerodynamic Decelerator Systems Technology Conference;2015-03-27

4. Investigation of Drag-Modulated Supersonic Inflatable Aerodynamic Decelerators for Sounding Rocket Payloads;Journal of Spacecraft and Rockets;2015-03

5. Aerothermal Environment and Thermal Response of Supersonic Inflatable Decelerators;53rd AIAA Aerospace Sciences Meeting;2015-01-03