000 00406pam a2200133a 44500
082 _aNASA
_bTN D-3064
100 _aLester,Harold C
245 1 _aA DESCRIBING-FUNCTION ANALYSIS OF THE STABILITY OF A LAUNCH VEHICLE WITH NONLINEAR THRUST VECTORING
260 _a
_bNasa, Washington, D.C.
_c1965
300 _a37
500 _aBound With Nasa Tn D-3061-63,3065-70
964 _gCIRC
997 _aTR15218 C
999 _c400316
_d400316