Spacecraft Recovery & Remote Sensing, Volume. 46, Issue 1, 11(2025)
The Effect of Structural Deformation on the Dynamic Stability of a Hypersonic Inflatable Aerodynamic Decelerator
[1] [1] BARTON R. Development of Attached Inflatable Decelerats f Supersonic Application: NASA CR66613[R]. Akron, OH, United States: Goodyear Aerospace Cpation, 1968.
[2] [2] HUGHES S J, DILLMAN R A, STARR B R, et al. Inflatable Reentry Vehicle Experiment(IRVE)Design Overiew[C]18th AIAA Aerodynamic Decelerat Systems Technology Conference Seminar, May 2326, 2005, Munich, Germany. [S. l.]: AIAA, 2005: AIAA 20051636. DOI: 10.25146.20051636.
[4] [4] O''KEEFE S, BOSE D. IRVEII PostFlight Trajecty Reconstruction[C]AIAA Atmospheric Flight Mechanics Conference, August 0205, 2010, Tonto, Ontario, Canada. [S. l.]: AIAA, 2009: AIAA 20107515. DOI: 10.25146.20107515.
[5] [5] JOSEPH D C, WALTER B, KAITLIN L, et al. Thermal Analysis Testing of Cidate Materials f PAIDAE Inflatable Aeroshell[C]20th AIAA Aerodynamic Decelerat Systems Technology Conference Seminar, May 47, 2009, Seattle, Washington. [S. l.]: AIAA, 2009: AIAA 20092925. DOI: 10.25146.20092925.
[14] [14] LINDELL M C, HUGHES S, DIXON M, et al. Structural Analysis Testing of the Inflatable Reentry Vehicle Experiment(IRVE)[C]47th AIAAASMEEAHS Structures, Structural Dynamics, Materials Conference, May 0104, 2006, Newpt, Rhode Isl. [S. l. ]: AIAA, 2006: AIAA 20061699. DOI: 10.25146.20061699.
[15] [15] LITTON D K, BOSE D M, CHEATWOOD F M, et al. Inflatable ReEntry Vehicle Experiment (IRVE)4 Overview[C]21st AIAA Aerodynamic Decelerat Systems Technology Conference Seminar, May 2326, Dublin, Irel. [S. l. ]: AIAA, 2011: AIAA 20112580. DOI: 10.25146.20112580.
[17] [17] LI L, GONYEA K, BRAUN R D. Finite Element Analysis of the Inflatable ReEntry Vehicle Experiment (IRVE)[C]56th AIAAEAHS Structures, Structural Dynamics, Materials Conference, January 59, 2015, Kissimmee, Flida. [S. l. ]: AIAA, 2015: AIAA 02042015. DOI: 10.25146.20150204.
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Xiaotian SHI, Guiru ZHANG, Meng LYU, Yuan ZHAO, Jun GAO. The Effect of Structural Deformation on the Dynamic Stability of a Hypersonic Inflatable Aerodynamic Decelerator[J]. Spacecraft Recovery & Remote Sensing, 2025, 46(1): 11
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Received: Oct. 11, 2024
Accepted: --
Published Online: Apr. 2, 2025
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