000 00489pam a2200133a 44500
082 _aNASA
_bTM X-179 -
100 _aFournier,Paul G
245 1 _aWIND-TUNNEL INVESTIGATION AT HIGH SUBSONIC SPEED OF THE STATIC LONGITUDINAL STABILITY CHARACTERISTICS OF A WINGED REENTRY VEHICLE HAVING A LARGE NEGATIVELY DEFLECTED FLAP-TYPE CONTROL SURFACE
260 _a
_bNasa, Washington, D.C.
_c1959
300 _a21
500 _aBound With Nasa Tm X-165-79
964 _gCIRC
997 _aTR8836 C
999 _c394791
_d394791