HIFiRE-5 Flight Vehicle Design
Author(s) -
Roger L. Kimmel,
David Adamczak,
Karen Berger,
Meelan M. Choudhari
Publication year - 2010
Publication title -
38th fluid dynamics conference and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2010-4985
Subject(s) - computer science , aeronautics , automotive engineering , engineering
The Hypersonic International Flight Research Experimentation (HIFiRE) program is a hypersonic flight test program executed by the Air Force Research Laboratories (AFRL) and Australian Defence Science and Technology Organization (DSTO). HIFiRE flight 5 is devoted to measuring transition on a three-dimensional body. This paper summarizes payload configuration, trajectory, vehicle stability limits and roughness tolerances. Results show that the proposed configuration is suitable for testing transition on a three-dimensional body. Transition is predicted to occur within the test window, and a design has been developed that will allow the vehicle to be manufactured within prescribed roughness tolerances
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