![]() ![]() 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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