Dimensioning of LV-RB type 3 missile and parameter study of RB behavior by simulating with a computer
Abstract
An approximate dimensioning of body and components of LV-RB missiles is discussed. A computer simulation with the continuous system modelling program (CSMP) was run, obtaining the performance characteristics for each case. Three types of missiles were considered, dependent upon target velocity and position. A set of charts and tables showing the estimated flight performance of the missiles is presented.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- July 1979
- Bibcode:
- 1979STIN...8017126A
- Keywords:
-
- Computer Design;
- Computerized Simulation;
- Flight Simulation;
- Missile Bodies;
- Missile Design;
- Air Defense;
- Missile Trajectories;
- Surface To Air Missiles;
- Launch Vehicles and Space Vehicles