Static Confirmation Tests - LGM-30G (Minuteman III)
Abstract
This document provides the final test report for the Structural Static Confirmation Tests of integrated structural components of the Minuteman LGM 30G missile. The primary purposes of the test program were to: (1) confirm structural compatibility of integrated structure, (2) determine ultimate load capability, (3) obtain load deflection characteristics. Static tests were conducted on integrated Stage III/PBV R and D and Operational stackups and Stage II Fwd/ II-III Interstage/Stage III stackup. Various critical combinations of external and internal pressure, axial load, moment, shear and heat were applied to the structure simulating the silo launch condition and powered flight conditions.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 07, 1969
- Accession Number
- AD0854544
Entities
People
- Gary D. Wonacott
- James E. Tancreto
- John Claus
- Wayne L. Salus
Organizations
- Boeing