NASA / TN D-990 -
Harris,Robert S
METHODS FOR DETERMINING THE OPTIMUM DESIGN OF STRUCTURES PROTECTED FROM AERODYNAMIC HEATING AND APPLICATION TO TYPICAL BOOST-GLIDE OR REENTRY FLIGHT PATHS
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.- Nasa, Washington, D.C., 1962
.- 37 .
Bound With Nasa Tn D-981-990
Author Added Entry:
Davidson,John R;
Copy Details:
Acc. No.: TR10027, Full Call No.: NASA TN D-990 -, Item type: Technical Report , Location: General Stacks,
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