American Institute of Aeronautics and Astronautics, American Society of Mechanical Engineers ... 42.5 50 2125 135 345 The specimen configuration consisted of a prefabricated layer of SLA ablator, 11-1/2 in. in diameter, which was bonded to a 0. ... to the heating rate and dynamic pressure of a low angle- low velocity Mars entry (Test Condition I) and of a high angle-high velocity entry ( Test Condition H).
|Title||:||A volume of technical papers presented at AIAA/ASME 8th Structures, Structural Dynamics, & Materials Conference, Palm Springs, California, March 29-31, 1967|
|Author||:||American Institute of Aeronautics and Astronautics, American Society of Mechanical Engineers|