000 00413pam a2200133a 44500
082 _aNASA
_bTN D-3283 -
100 _aMuraca,Ralph J
245 1 _aEMPIRICAL METHOD FOR DETERMINING STATIC DISTRIBUTED AERODYNAMIC LOADS ON AXISYMMETRIC MULTISTAGE LAUNCH VEHICLES
260 _a
_bNasa, Washington, D.C.
_c1966
300 _a104
500 _aBound With Nasa Tn D-3281-90
964 _gCIRC
997 _aTR10032 C
999 _c393146
_d393146