1Judy L Shin.Comparison of predicted and experimental real-gas pressure distributions on space shuttle orbiter nose for shuttle entry air data system.NASA-TP-1627,1980.
2Terry J Larson,Paul M.Use of nose cap and fuselage pressure orifices for determination of air data for space shuttle orbiter below supersonic speeds.NASA-TP-1643,1980.
3Stephen A Whitmore,Brent R Cobleigh,Edward A Haering.Design and calibration of the X-33 flush airdata sensing (FADS) system.AIAA 98-0201.
4Joel C Ellsworth,Stephen A Whitmore.Reentry air data system for a sub-orbital spacecraft based on X-34 design.AIAA 2007-1200.
5Joel C Ellsworth,Stephen A Whitmore.Simulation of a flush air-data system for transatmospheric vehicles.Journal of spacecraft and rocket,2008,45(4):716-732.
6Carlos Henrique Westhelle.X-38 backup air data system (AeroDAD).AIAA 2002-0007.
7Arthur C Grantz.X-37B orbital test vehicle and derivatives.AIAA 2011-7315.
8Christopher D Karlgaard,Roger E Beck,Stephen A O' Keefe,etc.Mars entry atmospheric data system modeling and algorithm development.AIAA 2009-3916.
9Soumyo Dutta,Robert D Braun,Christopher D Karlgaard.Atmospheric data system sensor placement optimization for mars entry,descent,and landing.AIAA 2012-4507.
10Mark C Davis,Joseph W Pahle,John Terry White,etc.Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at mach 3 to 8.AIAA 2000-0504.