Add to ORKGThe design and fabrication of a molded, coated fabric elbow joint capable of operating reliably at 8 psi internal pressure for extended periods of flexure is considered. The overall design of the joint includes: (1) selection of heatsettable fiber of sufficient strengths; (2) choosing an optimum fabric construction; (3) a fatigue resistant; flexible coating; and (4) a molding technique. A polyester yarn of type 56 Dacron and a urethane coating system were selected. The relationships between yarn and weave parameters which lead to an optimum fabric construction for the 8 psi elbow joint are defined
For use in hard space suits and the like, a joint between the torso covering and the upper arm cover...
Induction welding is an effective technique for joining unidirectional carbon fiber reinforced therm...
abstract: Current prosthetic designs have limitations with properly representing the full range of m...
Functional Requirements for spacesuit elbow joint:1) The system is a conformal, single-axis spacesui...
© The Author(s) 2022.Osteoarthritis is a chronic disease that affects joint cartilage and can cause ...
The National Aeronautics and Space Administration (NASA) Exploration Systems Mission Directorate ini...
This paper details the methodology for determining the joint factor for all parachute components. Th...
Eighteen bonded joint test specimens representing three different designs of a composite wing chordw...
Joints for use in interconnecting adjacent segments of an hermetically sealed spacesuit which have l...
A parachute joint is defined as a location where a component is sewn or connected to another compone...
Fabric, made of nylon ripstop coated with Neoprene, provides expansive and contractive mobility alon...
Uniform adhesive shear stress distributions in double-lap bonded joints and joint design criteri
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1959.Includes...
Plastic film is applied to each side of the fabric and the two films are then fused together with co...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1995.Includes...
For use in hard space suits and the like, a joint between the torso covering and the upper arm cover...
Induction welding is an effective technique for joining unidirectional carbon fiber reinforced therm...
abstract: Current prosthetic designs have limitations with properly representing the full range of m...
Functional Requirements for spacesuit elbow joint:1) The system is a conformal, single-axis spacesui...
© The Author(s) 2022.Osteoarthritis is a chronic disease that affects joint cartilage and can cause ...
The National Aeronautics and Space Administration (NASA) Exploration Systems Mission Directorate ini...
This paper details the methodology for determining the joint factor for all parachute components. Th...
Eighteen bonded joint test specimens representing three different designs of a composite wing chordw...
Joints for use in interconnecting adjacent segments of an hermetically sealed spacesuit which have l...
A parachute joint is defined as a location where a component is sewn or connected to another compone...
Fabric, made of nylon ripstop coated with Neoprene, provides expansive and contractive mobility alon...
Uniform adhesive shear stress distributions in double-lap bonded joints and joint design criteri
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1959.Includes...
Plastic film is applied to each side of the fabric and the two films are then fused together with co...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1995.Includes...
For use in hard space suits and the like, a joint between the torso covering and the upper arm cover...
Induction welding is an effective technique for joining unidirectional carbon fiber reinforced therm...
abstract: Current prosthetic designs have limitations with properly representing the full range of m...