Optimizing a Slingatron-Based Space Launcher Using MATLAB
Abstract
A slingatron is the name given to a propellantless mechanical means of launching a projectile. To date, slingatrons are only conceptual in nature, but their potential use as a ground-to-space launch mechanism for unmanned payloads is under investigation. Slingatrons can be configured in a variety of geometries; one form consists of a spiral track (or launch tube) that gyrates at a constant frequency about a set radius. Under proper conditions (design parameters), a projectile entering the spiral at its small-radius end will undergo nearly constant tangential acceleration before exiting. The differential equations governing the motion of the projectile within the spiral are highly non-linear, making the optimum design solution non-intuitive. This report describes how the slingatron works from first principles, then uses the numerical integration procedures within the computer software environment of Simulink(registered) and MatLab(registered) to search for and identify the optimum design solution parameters based on structural dynamics and mechanical design considerations.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 26, 2001
- Accession Number
- ADP012487
Entities
People
- G. Cooper
- M. Bundy
- S. Wilkerson
Organizations
- United States Army Research Laboratory