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):
Report Date:
1983-07-01
Pagination or Media Count:
89.0
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 Dynamics, Configurations and Control Surfaces
- Surface-Launched Guided Missiles
- Armor