![]() DELL OFL2 ELS OtLe TRANSITION =e anak, wk Sagtey Mt aġ 02060 2.3 O00 Weu0Fl2 040 9 0 0 UNKNOuN Pac-E 1 0F #21 MARTIN MISSILE TAIL EFFECTS Data As an aid in the use of theseĭata, tables that list the part numbers for the tabulated data from Tests Number 1 through 5Īnd the general list of nomenclature are repeated from Volume J at the end of this volume.ĪRWOLD ENGINEERING UEVELOPHENT CENTEX (ACDC) PROPULSION wlNO TUNNEL FACILITY(PWT) = AEROOYNAMIC WIND TUNNEL (OT) This volume contains the tabulated data that were obtained during (1) Tests Numberġ and 2 that were conducted in the Aerodynamic Wind Tunnel (4T) at AEDC duringĭecember 1970 and May 1972, respectively, and (2) Tests Number 3, 4, and 5 that wereĬonducted in the Unitary Plan Wind Tunnel (UPWT) at NASA Langley Research Centerĭuring March 1968, April 1970, and July 1971, respectively. ![]() ARO-PWT-TR-75-88) was submitted for publication on June 20, 1975. (NASA), Langley Air Force Base, Virginia. Laboratory, National Aeronautics and Space Administration ![]() Military hardware March 1976 other requests for thisĭocument must be referred to Air Force Armament Report contains information on test and evaluation of "ate \ \\ STATIC STABILITY AND FIN LOADS DATAįinal Report for Period March 1968 - March 1973ĭistribution limited to U.S. Tests Number 1 through 5"Īpproved for public release distribution isĭistribution authorized to U.S. Full text of " DTIC ADB010054: A Compilation of Static Stability and Fin Loads Data for Slender Body Missile Models with and without Tail Fins and Wings.
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