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Volumn , Issue , 2005, Pages

NASA research center contributions to space shuttle return to flight (SSRTF)

Author keywords

[No Author keywords available]

Indexed keywords

AEROTHERMAL; ANALYSIS TOOLS; DAMAGE ASSESSMENTS; DAMAGE CHARACTERIZATION; DAMAGE PROGRESSION; DESIGN CHANGE; EXPERIMENTAL TESTING; EXTERNAL TANKS; FOAM INSULATION; KEY SPACE; LANGLEY RESEARCH CENTERS; LEADING EDGE; MATERIAL CHARACTERISTICS; MATERIAL CHARACTERIZATIONS; NEW TECHNOLOGIES; NON DESTRUCTIVE EVALUATION; ON-ORBIT; REINFORCED CARBON-CARBON; REPAIR DECISIONS; RESEARCH CENTER; RETURN TO FLIGHT; SENSOR TECHNOLOGIES; SPACE SHUTTLE PROGRAMS; THERMAL PROTECTION SYSTEM; TRANSPORT ANALYSIS;

EID: 77957843299     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (2)

References (23)
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  • 6
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    • Weiser, Erik S.; St. Clair, Terry L.; and Nemeth, Michael P. Assessment of Technologies for the Space Shuttle External Tank Thermal Protection System and Recommendations for Technology Improvement - Part 1 : Materials Characterization and Analysis, NASA TM 2004-213238, July 2004.
    • Weiser, Erik S.; St. Clair, Terry L.; and Nemeth, Michael P. Assessment of Technologies for the Space Shuttle External Tank Thermal Protection System and Recommendations for Technology Improvement - Part 1 : Materials Characterization and Analysis, NASA TM 2004-213238, July 2004.
  • 7
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    • Application of Hilbert-Huang Transform for Improved Defect Detection in Terahertz NDE of Shuttle Tiles
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    • Anastasi, Robert F. and Madaras, Eric I. "Application of Hilbert-Huang Transform for Improved Defect Detection in Terahertz NDE of Shuttle Tiles", Presented at the SPIE International Symposia on Smart Structures and Materials/NDE, March 2005.
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  • 11
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    • Jackson, Karen E.; Fasanella, Edwin L.; Llye, Karen H.; and Spellman, Regina L. The Influence of Clocking Angle of the Projectile on the Simulated Impact Response on a Shuttle Leading Edge Wing Panel. NASA TM-2005213538, March 2005.
    • Jackson, Karen E.; Fasanella, Edwin L.; Llye, Karen H.; and Spellman, Regina L. The Influence of Clocking Angle of the Projectile on the Simulated Impact Response on a Shuttle Leading Edge Wing Panel. NASA TM-2005213538, March 2005.
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    • Jackson, Karen E.; Fasanella, Edwin L.; Lyle, Karen H.; and Spellman, Regina L. The Influence of Mesh Density on the Impact Response of a Shuttle Leading-Edge Wing Panel Finite Element Simulation, NASA TM2004-213501, November 2004.
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    • Assessment of LAURA for Laminar Supersonic Shallow Cavities
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    • (2004)
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    • Discrete Roughness Effects on the Shuttle Orbiter at Mach 6
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    • Berry, Scott and Hamilton, Harris. "Discrete Roughness Effects on the Shuttle Orbiter at Mach 6", AIAA Paper 2002-2714, June 2002.
    • (2002)
    • Berry, S.1    Hamilton, H.2
  • 19
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    • Computational Fluid Dynamics for Wing Re-Entry Vehicles at Hypersonic Conditions
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    • Reuther, James J.; Prabhu, Dinesh K.; Brown, James L.; Wright, Michael J.; and Saunders, David A. "Computational Fluid Dynamics for Wing Re-Entry Vehicles at Hypersonic Conditions", AIAA Paper 2004-2537, June 2004.
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    • Development of a Flexible Framework for Hypersonic Navier-Stokes Shuttle Orbiter Meshes
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    • (2004)
    • Alter, S.J.1    Reuther, J.J.2    McDaniel, R.D.3
  • 21
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    • Simulation of Flow Through Breach in Leading Edge at Mach 24
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.