The horizontal stabilizer of the 737 transport was redesigned. Five shipsets were fabricated using composite materials. Weight reduction greater than the 20% goal was achieved. Parts and assemblies were readily produced on production-type tooling. Quality assurance methods were demonstrated. Repair methods were developed and demonstrated. Strength and stiffness analytical methods were substantiated by comparison with test results. Cost data was accumulated in a semiproduction environment. FAA certification was obtained
The initial ground test of each component resulted in structural failure at less than ultimate desig...
The empennage component selected for this program is the vertical fin box of the L-1011 aircraft. Th...
Boeing's ATCAS program has completed its third year and continues to progress towards a goal to demo...
The development, testing, production activities, and associated costs that were required to produce ...
Results of tests conducted to demonstrate that composite structures save weight, possess long term d...
Activities related to development of an advanced composites stabilizer for the Boeing 737 commercial...
Activities related to development of an advanced composites stabilizer for the Boeing 737 commercial...
Detail design activities are reported for a program to develop an advanced composites elevator for t...
The 737 graphite-epoxy horizontal stabilizer was developed by Boeing as part of the NASA-ACEE (Aircr...
Detail design activities are reported for a program to develop an advanced composites elevator for t...
Under the NASA-sponsored contracts for Advanced Technology Composite Aircraft Structures (ATCAS) and...
The Advanced Technology Composite Aircraft Structures (ATCAS) program has studied transport fuselage...
The effort necessary to achieve a state of production readiness for the design and manufacturing of ...
Toppics addressed include: advanced composites on Boeing commercial aircraft; composite wing durabil...
Relationships between manufacturing costs and design details must be understood to promote the appli...
The initial ground test of each component resulted in structural failure at less than ultimate desig...
The empennage component selected for this program is the vertical fin box of the L-1011 aircraft. Th...
Boeing's ATCAS program has completed its third year and continues to progress towards a goal to demo...
The development, testing, production activities, and associated costs that were required to produce ...
Results of tests conducted to demonstrate that composite structures save weight, possess long term d...
Activities related to development of an advanced composites stabilizer for the Boeing 737 commercial...
Activities related to development of an advanced composites stabilizer for the Boeing 737 commercial...
Detail design activities are reported for a program to develop an advanced composites elevator for t...
The 737 graphite-epoxy horizontal stabilizer was developed by Boeing as part of the NASA-ACEE (Aircr...
Detail design activities are reported for a program to develop an advanced composites elevator for t...
Under the NASA-sponsored contracts for Advanced Technology Composite Aircraft Structures (ATCAS) and...
The Advanced Technology Composite Aircraft Structures (ATCAS) program has studied transport fuselage...
The effort necessary to achieve a state of production readiness for the design and manufacturing of ...
Toppics addressed include: advanced composites on Boeing commercial aircraft; composite wing durabil...
Relationships between manufacturing costs and design details must be understood to promote the appli...
The initial ground test of each component resulted in structural failure at less than ultimate desig...
The empennage component selected for this program is the vertical fin box of the L-1011 aircraft. Th...
Boeing's ATCAS program has completed its third year and continues to progress towards a goal to demo...