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.
Solid Rocket Motor Case Design and Test
2008
30 pages
Report
Keine Angabe
Englisch
Rockets , Unmanned Spacecraft , Launch vehicles , Rocket engine cases , Acceptance tests , Base lines , Fabrication , Fracture(mechanics) , Insulation , Nose cones , O rings , Requirements , Shells(structural forms) , Solid propellants , Structural components , Test and evaluation , Srmcs(solid rocket motor cases) , Elvs(expendable launch vehicles)
Advanced Solid Rocket Motor case design status
AIAA | 1993
|Advanced Solid Rocket Motor case design status
NTRS | 1993
|Solid rocket motor witness test
NTRS | 1991
|Solid rocket motor case summary.
NTRS | 1968
|Solid rocket motor case summary
AIAA | 1968
|