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Preliminary Results From First Flight of the Stratospheric Projectile Experiment of Entry Dynamics (SPEED)The dynamics of blunt-body vehicles in the transonic regime of atmospheric entry often play a dominant role in the design of atmospheric entry missions. Passage through these flight regimes can pose one of the greatest mission risks due to instabilities which can cause divergent and potentially catastrophic behavior. Most NASA entry missions encounter transonic dynamic stability challenges that drive system requirements and architecture choices.
Document ID
20240001359
Acquisition Source
Ames Research Center
Document Type
Abstract
Authors
C. D. Kazemba
(Ames Research Center Mountain View, United States)
B. J. Libben
(Ames Research Center Mountain View, United States)
H. S. Alper
(Ames Research Center Mountain View, United States)
Q. E. McKown
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
G. T. Swanson
(Ames Research Center Mountain View, United States)
M. C. Wilder
(Ames Research Center Mountain View, United States)
Date Acquired
January 30, 2024
Subject Category
Spacecraft Design, Testing and Performance
Aerodynamics
Meeting Information
Meeting: 21st International Planetary Probe Workshop (IPPW)
Location: Williamsburg, VA
Country: US
Start Date: June 8, 2024
End Date: June 9, 2024
Sponsors: Aix-Marseille University
Funding Number(s)
WBS: 258548.01.01.01
PROJECT: SCEX22024D (Dragonfly)
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Entry Vehicle
Dynamic Stability
Stratospheric Balloon
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