No	²File Name	¹Document Title
1	AIAA_1981-2512.pdf	OEX - Use of the Shuttle Orbiter as a Research Vehicle
2	AIAA_1992-3987.pdf	Shuttle Entry Aerothermodynamic Flight Research: The Orbiter Experiments (OEX) Program
3	AIAA_1999-0383.pdf	Flight Determined Subsonic Lift and Drag Characteristics of Seven Lifting-Body and Wing Body Reentry Vehicle Configurations With Truncated Bases
4	AIAA_1999-3560.pdf	X-33 Hypersonic Boundary Layer Transition
5	AIAA_1999-4160.pdf	Re-Entry Trajectory Planning for a Reusable Launch Vehicle
6	AIAA_2000-4388.pdf	An Object Oriented Design for Trim
7	AIAA_2000-5265.pdf	TCAT - A Tool For Automated Thermal Protection System Design
8	AIAA_2001-0352.pdf	Infrared Sensing Aeroheating Flight Experiment
9	AIAA_2002-2744.pdf	Discrete Roughness effects on Shuttle Orbiter at Mach 6
10	AIAA_2002-5171.pdf	Multidisciplinary Design Optimization to Future Space Transportation Vehicles
11	AIAA_2002-5265.pdf	A Study On Aerodynamic Performances of Lifting-Body Configurations for a Reentry Vehicle
12	AIAA_2002-5272.pdf	Plasma Formation During High Speed Flights in Upper Layers of the Earth's Atmosphere
13	NACA_TN-1956-3859.pdf	Comparison of flight and wind tunnel measurements of high speed airplane stability and control characteristics
14	NASA_17-5259.pdf	Operational Experience With Hypersonic Flight of the Space Shuttle
15	NASA_76N11131.pdf	An Experimental Summary of Plasma Arc Exposures of Space Shuttle High-Temperature Reusable Surface Insulation Tile Array With a Single Missing Tile
16	NASA_CP-1996-3256.pdf	Proceedings of the F8 Digital Fly-By-Wire and Super Critical Wing First Flights 20th Anniversary Celebration
17	NASA_CR-2001-211267.pdf	Inviscid Flow Computations of the Shuttle Orbiter for Mach 10 and 15 and Angle of Attack 40 to 60 Degrees
18	NASA_CR-2002-211249.pdf	Characterization of Subsystems for a WB-003 Single Stage Shuttle
19	NASA_RP-1992-1267.pdf	The High Resolution Accelerometer Package (HiRAP) Flight Experiment Summary for the First 10 Flights
20	NASA_TM-1985-85904.pdf	Impacts of Space Shuttle Thermal Protection System Tile on an F-15 Aircraft Vertical Tail
21	NASA_TM-1984-85907.pdf	Thermal Response of Space Shuttle Wing During Reentry Heating
22	NASA_TM-1984-85910.pdf	Active Control Technology Experience With the Space Shuttle in the Landing Regime
23	NASA_TM-1986-86030.pdf	Comparison of Pilot Effective Time Delay for Cockpit Controllers Used on Space Shuttle and Conventional Aircraft
24	NASA_TM-1987-86800.pdf	Effects of Forced and Free Convections on Structural Temperatures of Space Shuttle Orbiter During Reentry Flight
25	NASA_TM-1987-88276.pdf	Thermal Stress Analysis of Space Shuttle Orbiter Wing Skin Panel and Thermal Protection System
26	NASA_TM-1987-88278.pdf	Comparison of Flight-Measured and Calculated Temperatures on the Space Shuttle Orbiter
27	NASA_TM-1987-88281.pdf	Aircraft Parameter Estimation
28	NASA_TM-1987-88286.pdf	Thermal Stress Analysis of Space Shuttle Orbiter Subjected to Reentry Aerodynamic Heating
29	NASA_TM-1988-100438.pdf	In-Flight Rain Damage Tests of the Shuttle Thermal Protection System
30	NASA_TM-1989-4154.pdf	An In-Flight Technique for Wind Measurement in Support of the Space Shuttle Program
31	NASA_TM-1990-101701.pdf	Effects of Wing Sweep on In-Flight Boundary Layer Transition for a Laminar Flow Wing at Mach Numbers From O.60 to 0.79
32	NASA_TM-1990-4219.pdf	In-Flight Investigation of Shuttle Tile Pressure Orifice Installation
33	NASA_TM-1993-4499.pdf	Space Shuttle Hypersonic, Aerodynamic and Aerothermodynamic Flight Research and the Comparison to Ground Test Results
34	NASA_TM-1994-4495.pdf	Pressure Distributions on a 0.02-Scale Space Shuttle Orbiter Nose at Mach 21.5 in Helium
35	NASA_TM-1994-4633.pdf	Pressure-Sensing Performance of Upright Cylinders in a Mach 10 Boundary-Layer
36	NASA_TM-1995-104313.pdf	A Comparison of Hypersonic Vehicles Flight a Prediction Results
37	NASA_TM-1995-110165.pdf	Analytical Comparison of Three Stiffened Panel Concepts
38	NASA_TM-1995-110182.pdf	Orbiter Rarefied-Flow Reentry Measurements from the OARE on STS-062
39	NASA_TM-1996-104606.pdf	Dynamical Aspects of Climate Simulations Using the GEOS General Circulation Model
40	NASA_TM-1997-112866.pdf	Autonomous Modal Identification of the Space Shuttle Tail Rudder
41	NASA_TM-1997-4803.pdf	A Technique for Transient Thermal Testing of Thick Structures
42	NASA_TM-1997-4808.pdf	A Model for Space Shuttle Orbiter Tire Side Forces Based on NASA Landing Systems Research Aircraft Test Results
43	NASA_TM-1998-206540.pdf	Design and Calibration of the X-33 Flush Airdata Sensing (FADS) System
44	NASA_TM-1998-206555.pdf	Thermal Analysis of a Metallic Wing Glove for a Mach-8 Boundary-Layer Experiment
45	NASA_TM-2000-209015.pdf	A Real-Time Method for Estimating Viscous Forebody Drag Coefficients
46	NASA_TM-2004-213256.pdf	Assessment of Technologies for the Space Shuttle External Tank Thermal Protection System and Recommendations for Technology Improvement
47	NASA_TP-1980-1643.pdf	Use of Nose Cap and Fuselage Pressure Orifices for Determination of Air Data for Space Shuttle Orbiter Below Super Sonic Speeds
48	NASA_TP-1982-2011.pdf	Effects of Wing-Leading-Edge Modifications on a Full-Scale, Low-Wing General Aviation Airplane
49	NASA_TP-1986-2657.pdf	Finite Element Reentry Heat-Transfer Analysis of Space Shuttle Orbiter
50	NASA_TP-2000-209034.pdf	A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High-Speed Aircraft
51	NASA_TP-2002-210771.pdf	Reentry Vehicle Flight Controls Design Guidelines: Dynamic Inversion
1.) All files are also available from the Dryden Technical Reports Server. (File names have been altered to conform to site standards) 2.) Due to a shortage of web space not all of the reports are directly available. If a report is not downloadable contact this site and it will either be sent to you via e-mail or made available.