Accession Number : ADA139130

Title :   Pershing II Simulation Studies. Debris Dynamics and 2.75 Rocket 6-DOF (Degree of Freedom).

Descriptive Note : Final rept.,

Corporate Author : ALABAMA UNIV IN HUNTSVILLE SCHOOL OF ENGINEERING

Personal Author(s) : Tilley,P A ; Hall,D A

PDF Url : ADA139130

Report Date : Jul 1983

Pagination or Media Count : 89

Abstract : Pershing II simulation studies were performed using the program MSIXB1 during this task. Analysis and documentation of MSIXB1 and the 2.75 6-DOF simulation were completed for future use in debris studies. (Author)

Descriptors :   *Ballistic trajectories, *Guided missile components, *Rockets, *Debris, *Impact point, *Impact prediction, *Computerized simulation, *Computer programs, Second stage engines, Adapters, Dynamics, Tracking, Flight testing, Input output processing, Flow charting, Subroutines, Plotting, Models, Approximation(Mathematics), Statistical analysis, Surface to surface, Air to surface, Coordinates, Helicopters, Aerodynamics, Rocket trajectories, Guided missile trajectories, Guided missiles, Algorithms, Coefficients, Degrees of freedom

Subject Categories : Computer Programming and Software
      Guided Missile Dynam, Config & Cntrl Surfaces
      Surface-launched Guided Missiles
      Armor

Distribution Statement : APPROVED FOR PUBLIC RELEASE