Radiant heating simulation Second phase report, 10 Nov. - 30 Dec. 1964
Radiant heater technology for simulation of radiant heating associated with spacecraft atmospheric entry
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Radiant heater technology for simulation of radiant heating associated with spacecraft atmospheric entry
Supersonic inviscid flow of equilibrium real gas over blunt axisymmetric bodies at large angles of attack including Apollo and Gemini shapes
Simultaneous fabrication of enhancement mode metal oxide semiconductor transistors in epitaxial material
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Ion introduction into strong fields of quadrupole mass spectrometer