Accession Number : AD0434302


Title :   STRENGTH ANALYSIS OF THE NAVAIRDEVCEN C.G. TARGET LAUNCHER.


Descriptive Note : Final rept.,


Corporate Author : NAVAL AIR DEVELOPMENT CENTER JOHNSVILLE PA ENGINEERING DEVELOPMENT LAB


Personal Author(s) : Lobel,Seymour Z


Report Date : 18 Mar 1964


Pagination or Media Count : 13


Abstract : A structural analysis is presented for the LAU37/A center-of-gravity (c.g.) launcher and associated wing fitting adapters for F-8 aircraft. The adapters are designed for interchangeable employment of an LAU-37/A or Aero 38B launcher. The LAU-37/A launcher is designed for carrying, launching, and recovering TA-7, -5T, and TDU-22/B type c.g. -towed targets with F-8 aircraft. (Author)


Descriptors :   *JET FIGHTERS , *AERIAL TARGETS , TOWED BODIES , ATTACHMENT , GRAVITY , AIRCRAFT PROTUBERANCES , EXTERNAL STORES , LAUNCHING , RECOVERY , SUBSONIC CHARACTERISTICS , LOADS(FORCES) , DISTRIBUTION , FLIGHT TESTING , ACCEPTABILITY , ADAPTERS , STRUCTURES , STRUCTURAL COMPONENTS , WINGS


Distribution Statement : APPROVED FOR PUBLIC RELEASE