The space shuttle development program provided the opportunity to challenge many of the established practices and approaches used in prior manned space flight programs. The most significant accomplishments and resulting precedents which emerged during the structural development of the space shuttle and the space shuttle orbiter are reviewed. Innovations in criteria, design solutions, and certification are highlighted, and brief comments on the lessons learned are included. Thermal stress, graphite epoxy moisture, window structure, and structural inspection are discussed under lessons learned
The application of general design approaches for preventing failures due to repeated load cycles is ...
The space shuttle introduced a new dimension in the complexity of the structural dynamics of a space...
The planned missions for the space shuttle dictated a unique and technology-extending rocket engine....
The major material and design challenges associated with the orbiter thermal protection system (TPS)...
The principal design issues, tests, and analyses required to solve the tile integrity problem on the...
The evolution of the orbiter aft heat shield seal (AHSS) design, which involved advancing mechanical...
Major mechanical systems of the Orbiter space vehicle are summarized with respect to general design ...
Alternate thermal protection system (TPS) concepts to the Space Shuttle Orbiter were assessed. Metal...
The major aerodynamic design challenge at the beginning of the United States Space Transportation Sy...
The Space Shuttle Orbiter is in the final stages of preparation, proceeding toward mating with the o...
Considerable progress has been made in designing the Space Shuttle orbiter and defining its subsyste...
The development and testing of primary structural elements that are necessary to design a windshield...
The space shuttle orbiter atmospheric revitalization subsystem provides thermal and contaminant cont...
A study program was conducted to determine the nondestructive evaluation (NDE) requirements and to d...
The Space Shuttle orbiter's thermal protection system (TPS), designed mainly on the basis of wind tu...
The application of general design approaches for preventing failures due to repeated load cycles is ...
The space shuttle introduced a new dimension in the complexity of the structural dynamics of a space...
The planned missions for the space shuttle dictated a unique and technology-extending rocket engine....
The major material and design challenges associated with the orbiter thermal protection system (TPS)...
The principal design issues, tests, and analyses required to solve the tile integrity problem on the...
The evolution of the orbiter aft heat shield seal (AHSS) design, which involved advancing mechanical...
Major mechanical systems of the Orbiter space vehicle are summarized with respect to general design ...
Alternate thermal protection system (TPS) concepts to the Space Shuttle Orbiter were assessed. Metal...
The major aerodynamic design challenge at the beginning of the United States Space Transportation Sy...
The Space Shuttle Orbiter is in the final stages of preparation, proceeding toward mating with the o...
Considerable progress has been made in designing the Space Shuttle orbiter and defining its subsyste...
The development and testing of primary structural elements that are necessary to design a windshield...
The space shuttle orbiter atmospheric revitalization subsystem provides thermal and contaminant cont...
A study program was conducted to determine the nondestructive evaluation (NDE) requirements and to d...
The Space Shuttle orbiter's thermal protection system (TPS), designed mainly on the basis of wind tu...
The application of general design approaches for preventing failures due to repeated load cycles is ...
The space shuttle introduced a new dimension in the complexity of the structural dynamics of a space...
The planned missions for the space shuttle dictated a unique and technology-extending rocket engine....