Estimating Orion Heat Shield Failure due to Ablator Cracking von Vander Kam, Jeremy C, Gage, Peter

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Reduced-order high-fidelity methodologies for the design of civil transport high-lift systems / by Jeremy C. Vander Kam von Vander Kam, Jeremy C

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Estimating Orion Heat Shield Failure Due To Ablator Cracking During The EFT-1 Mission von Vander Kam, Jeremy C., Gage, Peter

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A Reliability Comparison of Classical and Stochastic Thickness Margin Approaches to Address Material Property Uncertainties for the Orion Heat Shield von Sepka, Steven A., McGuire, Mary Kathleen, Vander Kam, Jeremy C.

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Ablators for Human and Robotic Exploration of the Moon, Mars and Beyond von Venkatapathy, Ethiraj, Beck, Robin A., Gage, Peter J., Vander Kam, Jeremy C.

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3D Woven Mid-Density Carbon Phenolic (3MDCP) Full-Scale Heatshield Development for Mars Sample Return (MSR) Earth Entry System (EES) von Marshall, Peter Edward, Ellerby, Donald T, Peterson, Keith Hoppe, Nishioka, Owen, Kam, Jeremy C Vander

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Ablative Thermal Protection System (TPS) Margin Study von Rickman, Steven L, Green, Lawrence, Remark, Brian J, Bouslog, Stanley A, Kam, Jeremy C Vander, Khalessi, Mohammed

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Sustaining Thermal Protection Systems Needed for Uranus Probes von Venkatapathy, Ethiraj, Ellerby, Donald T, Gasch, Matthew J, Stackpoole, Margaret Mary, Monk, Joshua D, Kam, Jeremy C Vander, Alpert, Hannah

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Mars Sample Return – An Overview of the Capture, Containment and Return System von Cataldo, Giuseppe, Feehan, Thomas Brendan, Pellerano, Fernando A, Mukherjee, Suparna, Lin, Justin Y, Szalai, Christine E, Childs, Brian W, Corliss, James M, Neuman, Mark A, Sarli, Bruno Victorino, Teeney, Leo, Kam, Jeremy C Vander, White, Todd Richard, Yew, Calinda Macy, Zumwalt, Carlie H, Teeney, Leo

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