000 00436pam a2200133a 44500
082 _aNASA
_bTN D-1389 -
100 _aNewsom,Jr,William A
245 1 _aFORCE-TEST INVESTIGATION OF THE STABILITY AND CONTROL CHARACTERISTICS OF A FOUR-PROPELLER TILT-WING VTOL MODEL WITH A PROGRAMED FLAP
260 _a
_bNasa, Washington, D.C.
_c1962
300 _a55
500 _aBound With Nasa Tn D-1381-90
964 _gCIRC
997 _aTR9557 C
999 _c395184
_d395184