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Autor:
Eric Slimko, Kristina Skokova, Jarvis T. Songer, Chun Tang, David M. Driver, J. Enrique Carballo, Alan M. Cassell, Helen H. Hwang, Dinesh K. Prabhu, Jose A. Santos, William H. Willcockson, Robin Beck
Publikováno v:
Journal of Spacecraft and Rockets. 51:1151-1166
Thermal protection system materials for the Mars Science Laboratory mission were tested in the NASA Ames 60 MW arcjet in a shear environment. Shear tests were performed on candidate ablative heat shield materials in wedge and swept cylinder test fixt