Add to ORKGDesign studies involving weight and cost were carried out for several structural concepts applicable to space shuttle disposable tankage. An effective design, a honeycomb stabilized pressure vessel, was chosen. A test model was designed and fabricated
On the composite cryotank technology development (CCTD) project, the Boeing Company built two cryota...
To achieve NASA's mission of space exploration, innovative manufacturing processes are being applied...
An integrated, generic unibody composite pressurized structure (UCPS) combined with a positive expul...
A study of thread-reinforced polyurethane foam and glass fabric liner, serving as internally bonded ...
The use of high strength and modulus of advanced filamentary composites to reduce the structural wei...
The Engineering Guide presents curves and general equations for safelife design of lightweight glass...
The Nonmetallic Materials and Processes Group is presently working on several projects to optimize c...
NASA sponsored composites research and development programs were set in place to develop the critica...
Two different Kevlar-49 filament-reinforced metal sphere designs were developed, and six vessels of ...
This paper proposes a new type of configuration to support the propellant tanks in large size spacec...
The development of metal structures reinforced with filamentary composites as a weight saving featur...
This experimental program was undertaken to establish a fracture control method for composite tanks ...
Intertanks, the structure between tanks of launch vehicles, are prime candidates for weight reductio...
The Composite Cryotank Technologies and Demonstration (CCTD) project substantially matured composite...
Design, analysis, and fabrication studies were performed on nonintegral (suspended) tanks using a re...
On the composite cryotank technology development (CCTD) project, the Boeing Company built two cryota...
To achieve NASA's mission of space exploration, innovative manufacturing processes are being applied...
An integrated, generic unibody composite pressurized structure (UCPS) combined with a positive expul...
A study of thread-reinforced polyurethane foam and glass fabric liner, serving as internally bonded ...
The use of high strength and modulus of advanced filamentary composites to reduce the structural wei...
The Engineering Guide presents curves and general equations for safelife design of lightweight glass...
The Nonmetallic Materials and Processes Group is presently working on several projects to optimize c...
NASA sponsored composites research and development programs were set in place to develop the critica...
Two different Kevlar-49 filament-reinforced metal sphere designs were developed, and six vessels of ...
This paper proposes a new type of configuration to support the propellant tanks in large size spacec...
The development of metal structures reinforced with filamentary composites as a weight saving featur...
This experimental program was undertaken to establish a fracture control method for composite tanks ...
Intertanks, the structure between tanks of launch vehicles, are prime candidates for weight reductio...
The Composite Cryotank Technologies and Demonstration (CCTD) project substantially matured composite...
Design, analysis, and fabrication studies were performed on nonintegral (suspended) tanks using a re...
On the composite cryotank technology development (CCTD) project, the Boeing Company built two cryota...
To achieve NASA's mission of space exploration, innovative manufacturing processes are being applied...
An integrated, generic unibody composite pressurized structure (UCPS) combined with a positive expul...