Add to ORKGCalculated ablative quantities for nylon phenolic heat shielding materials of hyperbolic reentry veh...
Structural analysis of Apollo aft heat shield under water impact loading condition
Apollo/Saturn I unmanned space flight to test command module ablative heat shiel
Launch vehicle flight tests of effects of Apollo heat shield irregularities on ablative material per...
Ablation behavior of heat shield of Apollo command module over wide range of thermal environment
Wind tunnel study of aerodynamic pressures on Apollo command module configuratio
Impact water pressures, accelerations, and landing dynamics of scale model Apollo command module wit...
The Apollo program offered the first opportunity to obtain aerothermodynamic measurements at superor...
Radio frequency transmission characteristics of ablation materials for planetary entry vehicle heat ...
Sensors measure surface erosion rate of ablating material in reentry vehicle heat shield. Each senso...
The aerodynamic and aerothermal heating at the leeward surfaces of the Apollo capsule flying high an...
Protuberances, cavities, and angle of attack effect on wind tunnel pressure and heat transfer distri...
Carbon-phenolic material consisting of 50 percent carbon fibers and 50 percent phenolic resin was fl...
Results are presented from an investigation to determine the effects of fabrication-induced defects ...
Design and operation of make wire, light pipe, and spring wire sensors to measure in-flight thermal ...
Calculated ablative quantities for nylon phenolic heat shielding materials of hyperbolic reentry veh...
Structural analysis of Apollo aft heat shield under water impact loading condition
Apollo/Saturn I unmanned space flight to test command module ablative heat shiel
Launch vehicle flight tests of effects of Apollo heat shield irregularities on ablative material per...
Ablation behavior of heat shield of Apollo command module over wide range of thermal environment
Wind tunnel study of aerodynamic pressures on Apollo command module configuratio
Impact water pressures, accelerations, and landing dynamics of scale model Apollo command module wit...
The Apollo program offered the first opportunity to obtain aerothermodynamic measurements at superor...
Radio frequency transmission characteristics of ablation materials for planetary entry vehicle heat ...
Sensors measure surface erosion rate of ablating material in reentry vehicle heat shield. Each senso...
The aerodynamic and aerothermal heating at the leeward surfaces of the Apollo capsule flying high an...
Protuberances, cavities, and angle of attack effect on wind tunnel pressure and heat transfer distri...
Carbon-phenolic material consisting of 50 percent carbon fibers and 50 percent phenolic resin was fl...
Results are presented from an investigation to determine the effects of fabrication-induced defects ...
Design and operation of make wire, light pipe, and spring wire sensors to measure in-flight thermal ...
Calculated ablative quantities for nylon phenolic heat shielding materials of hyperbolic reentry veh...
Structural analysis of Apollo aft heat shield under water impact loading condition
Apollo/Saturn I unmanned space flight to test command module ablative heat shiel