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Volumn , Issue , 2003, Pages

Assessing factors of safety, margins of safety, and reliability of thermal protection systems

Author keywords

[No Author keywords available]

Indexed keywords

DESIGN APPROACHES; DESIGN-RELIABILITY; ENTRY VEHICLES; FACTOR OF SAFETY; FACTORS OF SAFETIES; RELIABILITY METHODS; STAGNATION POINTS; THERMAL PROTECTION SYSTEM;

EID: 84896769004     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (6)

References (13)
  • 1
    • 84896803001 scopus 로고    scopus 로고
    • Summary of the Mars Exploration Rover Aeroshell Critical Design Review
    • May 30-31
    • Summary of the Mars Exploration Rover Aeroshell Critical Design Review, JPL, May 30-31, 2001
    • (2001) JPL
  • 2
    • 21344490499 scopus 로고
    • Risk Management for the Tiles of the Space Shuttle
    • Jan-Feb
    • M. E. Pate-Cornell and P. S. Fischbeck, "Risk Management for the Tiles of the Space Shuttle", Interfaces, Vol 24, No. 1, Jan-Feb, 1994, pp. 64-86
    • (1994) Interfaces , vol.24 , Issue.1 , pp. 64-86
    • Pate-Cornell, M.E.1    Fischbeck, P.S.2
  • 3
    • 84896784593 scopus 로고
    • Probabilistic Risk Asssessment of the Space Shuttle: A Study of the Potential of Losing the Vehicle During Nominal Operations, Volume I Final Report
    • Feb
    • J. R. Fragola et al, "Probabilistic Risk Asssessment of the Space Shuttle: A Study of the Potential of Losing the Vehicle During Nominal Operations, Volume I Final Report", SAIC/NY95-02-05, Feb. 28, 1995
    • (1995) SAIC/NY95-02-05 , pp. 28
    • Fragola, J.R.1
  • 4
    • 84884627971 scopus 로고    scopus 로고
    • Effects of Aerodynamic Heating and TPS Thermal Performance Uncertainties On the Shuttle Orbiter
    • W. D. Goodrich, S. M. Derry, and R. J. Maraia, "Effects of Aerodynamic Heating and TPS Thermal Performance Uncertainties on the Shuttle Orbiter", in Entry Heating and Thermal Protection, edited by W. B. Olstad, Progress in Astronautics and Aeronautics, Vol. 69.
    • Entry Heating and Thermal Protection , vol.69
    • Goodrich, W.D.1    Derry, S.M.2    Maraia, R.J.3
  • 7
    • 0031100517 scopus 로고    scopus 로고
    • Trajectory-Based Validation of the Shuttle Heating Environment
    • March- April
    • D. Olynick and T. Tam, "Trajectory-Based Validation of the Shuttle Heating Environment", J of Spacecraft and Rockets, Vol. 34, No. 2, March- April, 1997
    • (1997) J of Spacecraft and Rockets , vol.34 , Issue.2
    • Olynick, D.1    Tam, T.2
  • 8
    • 0032632115 scopus 로고    scopus 로고
    • Mars Pathfinder Entry Temperature Data, Aerothermal Heating, and Heatshield Material Response
    • May-June
    • Milos et. al., "Mars Pathfinder Entry Temperature Data, Aerothermal Heating, and Heatshield Material Response", J. of Spacecraft and Rockets, Vol. 36, No. 3, pp 380-391, May-June, 1999
    • (1999) J. of Spacecraft and Rockets , vol.36 , Issue.3 , pp. 380-391
    • Milos1
  • 10
    • 0032652865 scopus 로고    scopus 로고
    • Analysis of Galileo Probe Heatshield Ablation and Temperature Data
    • May-June
    • F. S. Milos, et al, "Analysis of Galileo Probe Heatshield Ablation and Temperature Data", J. of Spacecraft and Rockets, Vol. 34, No. 3, May-June, 1999, pp. 298-306
    • (1999) J. of Spacecraft and Rockets , vol.34 , Issue.3 , pp. 298-306
    • Milos, F.S.1
  • 11
    • 0031276477 scopus 로고    scopus 로고
    • Galileo Probe Heatshield Ablation Experiment
    • F. S. Milos, "Galileo Probe Heatshield Ablation Experiment", J. of Spacecraft and Rockets, Vol. 34, No. 6, 1997, pp. 705-713
    • (1997) J. of Spacecraft and Rockets , vol.34 , Issue.6 , pp. 705-713
    • Milos, F.S.1
  • 12
    • 84896790320 scopus 로고    scopus 로고
    • Estimates of the Orbiter Thermal Protection System Reliability
    • June
    • P. Kolodziej, D. J. Rasky, E. Venkatapathy, "Estimates of the Orbiter Thermal Protection System Reliability", AIAA 2003-3766, June, 2003
    • (2003) AIAA 2003-3766
    • Kolodziej, P.1    Rasky, D.J.2    Venkatapathy, E.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.