Terminal Homing Guidance for the Shoulder Launched Direct Fire Missile.
Abstract
This 10 month program derived the conceptual design of a small diameter, shoulder launched, direct fire missile for use as a guidance test bed. The resulting design is practical, versatile, and modular, and can exercise a variety of present and advanced technology seekers over a broad range regime. Although the missile makes maximum use of off-the-shelf components and is well within existing technology capabilities, its accuracy potential is sufficient for any anticipated guidance system.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 01, 1975
- Accession Number
- ADA010741
Entities
People
- R. C. Scott
Organizations
- Martin Marietta