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 |