The objective of the engineering design study of the close air support weapon (CASW) was to provide design considerations for the new close air support missile (CASM). The derivation of the missile was undertaken based on the modification of an existing missile. This study incorporates operational requirement and warhead effectiveness studies for various close air support targets leading to warhead and launch envelope recommendations. A thorough analysis of the system performance and terminal accuracy was conducted. Missile simulation models and a system description, including missile, launcher, avionics, and aerospace ground equipment (AGE) are provided.
Close Air Support Weapon Engineering Design Study. Volume VI. Missile Simulation
1971
114 pages
Report
No indication
English
Missile Technology , Air to surface missiles , Tactical air support , Close support , Design , Models(Simulations) , Computer programs , Systems engineering , Guided missile launchers , Ground support equipment , Monte carlo method , Digital computers , Flow charting , Compilers , Subroutines , Automatic pilots , Aerodynamic characteristics , Aerodynamic control surfaces , Light homing , Lasers , Miss distance , Transformations(Mathematics) , Avionics , Casw(Close air support weapons) , Casm(Close air support missiles) , Close air support weapons , Close air support missiles , Computer aided design , Fortran , Fortran 4 programming language , Ge 635 computers , Maverick missiles , Missile modification , Sadsam computer
Drone intelligence munitions and flight vehicle for close-in weapon system against missile
European Patent Office | 2018
|