The X-43A flush airdata sensing system flight test results

AIAA Atmospheric Flight Mechanics Conference and Exhibit

Volumn , Issue , 2008, Pages

  Baumann, Ethan ^a,c   Pahle, Joseph W ^a,c   Davis, Mark C ^a,d   White, John Terry ^b,e  

^a NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

^b Tybrin Corporation   (United States)

^c Mail Stop 4840D   (United States)

^d Aerodynamics and Propulsion Branch   (United States)

^e MS 4830D ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ESTIMATION ALGORITHM; FLIGHT CONTROL; FLIGHT TEST; FLIGHT TEST DATA; HYPER-X; HYPERSONIC SPEED; NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONS; PRESSURE DATA; RESEARCH VEHICLES; SENSING SYSTEMS;

AERODYNAMICS; ALGORITHMS; ESTIMATION; MECHANICS; NASA; SENSORS;

HYPERSONIC VEHICLES;

EID: 75749119524     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

1. Davis, M. C., Pahle, J. W., White, J. T., Marshall, L. A., Mashburn, M. J., and Franks, R., "Development of a Flush Airdata Sensing System on a Sharp-Nosed Vehicle for Flight at Mach 3 to 8," NASA/TM-2000-209017, May 2000.
2. Freeman, D. C., Jr., Reubush, D. E., McClinton, C. R., Rausch, V. L., and Crawford, J. L., "The NASA Hyper-X Program,"NASA/TM-1997-207243, Oct. 1997.
3. Ferlemann, S. M., McClinton, C. R., Rock, K. E., and Voland, R. T., "Hyper-X Mach 7 Scramjet Design, Ground Test and Flight Results," AIAA-2005-3322, May 2005.
4. X-43A Mishap Investigation Board, "Report of Findings: X-43A Mishap," Vol. I, May 2003.
5. Marshall, L. A., Corpening, G. P., and Sherrill, R., "A Chief Engineer's View of the NASA X-43A Scramjet Flight Test," AIAA-2005-3332, May 2005.
6. Marshall, L. A., Bahm, C., Corpening, G. P., and Sherrill, R., "Overview With Results and Lessons Learned of the X-43A Mach 10 Flight," AIAA-2005-3336, May 2005.
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8. Baumann, E., Bahm, C., Strovers, B., and Beck, R., "The X-43A Mach 10 Mission Guidance and Control Updates, Rationale, and Flight Test Results," NASA/TM-2007-214610, Jan. 2007. Available from the former chief engineer, X-43 Project.
9. Ohlhorst, C. W., Glass, D. E., Bruce, W. E., Lindell, M. C., Vaughn, W. L., Smith, R. W., Dirling, R. B., Jr., Hogenson, P. A., Nichols, J. M., Risner, N. W., Thompson, D. R., Kowbel, W., Sullivan, B. J., Koenig, J. R., and Cuneo, J. C., "Development of X-43A Mach 10 Leading Edges," IAC-05-D2.5.06, Oct. 2005.
10. Morelli, E. A., Derry, S. D., and Smith, M. S., "Aerodynamic Parameter Estimation for the X-43A (Hyper-X) from Flight Data," AIAA-2005-5921, Aug. 2005.
11. Baumann, E. A., "Tailored Excitation for Frequency Response Measurement Applied to the X-43A Flight Vehicle," NASA/TM-2007-214609, Jan. 2007.
12. White, J. T., "Results of the HYPER-X Research Vehicle (HXRV) Flush Air Data Sensing (FADS) System Wind Tunnel Test (AEDC VA435)," HX-DFRC-0308, Dec. 2003.
13. Karlgaard, C. D., Tartabini, P. V., Blanchard, R. C., Kirsch, M., and Toniolo, M. D., "Hyper-X Post-Flight-Trajectory Reconstruction," Journal of Spacecraft and Rockets, Vol. 43, No. 1, January-February 2006.
14. Karlgaard, C. D., Martin, J. G., Tartabini, P. V., and Thornblom, M. N., "Hyper-X Mach 10 Trajectory Reconstruction," AIAA-2005-5920, Aug. 2005.