Flush Air Data Sensing System for a Sharp-Nosed Hypersonic Vehicle with Curved-Wedge Forebody
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Kakuda 981-1525, Japan
Funder
Acquisition, Technology and Logistics Agency
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference26 articles.
1. Design and calibration of the X-33 Flush Airdata Sensing (FADS) system
2. CobleighB. R.WhitmoreS. A.HaeringE. A.BorrerJ.RobackV. E. “Flush Airdata Sensing (FADS) System Calibration Procedures and Results for Blunt Forebodies,” NASA TP-1999-209012, Nov. 1999.
3. In-flight demonstration of a real-time flush airdata sensing (RT-FADS) system
4. WhitmoreS. A.MoesT. R.LarsonT. J. “Preliminary Results from a Subsonic High Angle-of-Attack Flush Airdata Sensing (HI-FADS) System: Design, Calibration, and Flight Test Evaluation,” NASA TM-101713, Jan. 1990;
5. also AIAA Paper 1990-0232, 1990.
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