The technology with respect to fracture control requirements of the shuttle is considered. The current state-of-the-art does permit an approach based on linear elastic fracture mechanics concepts. Development and implementation of a fracture control plan should recognize deficiencies and provide adequate resources for the extensive empirical test data which are required. With respect to the cost impact of such tests, recent experiences involving advanced aircraft systems have seen unit cost increases of from 200 to 500 percent.
Development of methods for fracture control of space shuttle structures
1972-07-01
Conference paper
No indication
English
Space Shuttle Orbiter Fracture Control Plan
NTRS | 1974
|Space Shuttle Orbiter Fracture Control Plan
NTIS | 1973
Space Shuttle Orbiter Fracture Control Plan
NTRS | 1973
|