Accession Number : AD0854199

Title :   Tactical Missile Launcher Feasibility Study. Book II.

Descriptive Note : Final rept.

Corporate Author : HONEYWELL INC HOPKINS MINN ORDNANCE DIV

Report Date : 1968

Pagination or Media Count : 241

Abstract : The document contains inertial load tables and air load tables relative to the development and the results of a study of the feasibility of designing a standard tactical missile launcher which is capable of carrying and launching hypothetical stores, weighing from 500 to 3,000 pounds, from the F100, F101, F104 and F105 aircraft.

Descriptors :   (*JET FIGHTERS, GUIDED MISSILE LAUNCHERS), (*GUIDED MISSILE LAUNCHERS, FEASIBILITY STUDIES), TACTICAL BOMBING, AIR TO SURFACE MISSILES, GUIDED MISSILE TRAJECTORIES, AERODYNAMIC LOADING, AERODYNAMIC CHARACTERISTICS, EXTERNAL STORES, COMPUTER PROGRAMMING, MATHEMATICAL MODELS, EQUATIONS OF MOTION, NUMERICAL METHODS AND PROCEDURES, TABLES(DATA)

Subject Categories : Attack and Fighter Aircraft
      Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE