Solid Rocket Motor Case Design and Test
Abstract
This standard establishes baseline requirements for the design, fabrication, qualification and acceptance tests, and inspections of the solid rocket motor cases (SRMCs) of launch vehicles. An SRMC consists of the outer shell and the associated factory and field joints. The associated aft skirt, nose cone, and other structural components are not included. Solid propellants, insulators and other nonstructural components, such as O-rings, are also not included.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 13, 2008
- Accession Number
- ADA633328
Entities
Organizations
- Air Force Space Command