Add to ORKGPressure pulses, shock and vibratory loading on launch vehicle connectors - heat environment, vacuum and radiation effects on connector gasket
In Stennis Space Center's Component Test Facility, piping lines carry rocket propellants and high pr...
Polyimide second-stage rod seals were evaluated to determine their suitability for applications in s...
The assembly joints of modem solid rocket motor cases are generally sealed using conventional O-ring...
Design criteria for zero-leakage connectors for launch vehicles - plastic flow & flange rollin
Mathematical model of interface sealing phenomenon in determining design criteria for zero leakage c...
Principles of connector testing, design evaluation of commercial connectors, and assessment of desig...
Extremely fine finished surfaces as mating parts for sealing in fluid connectors and statistical ana...
Aerospace technology and design considerations for leak-tight separable, semipermanent, and permanen...
Flow control of cryogenic liquids is achieved through use of an electrical feed-through connector wi...
U-tube containing liquid indicates pressure differences in a leakage tester. This tube, connecting t...
Selection of materials for electrical connectors compatible with future space mission
Guide manual for aiding designers in selection of duct, tubing, and gasketing materials for space ve...
The assembly of flanges, seals, and pipes are used to carry cryogenic fluid from a storage tank to t...
An analytical method and a design procedure to develop flanged separable pipe connectors are discuss...
Three types of surface conditions (plain surface, plain surface with oxidation inhibitor, and toothe...
In Stennis Space Center's Component Test Facility, piping lines carry rocket propellants and high pr...
Polyimide second-stage rod seals were evaluated to determine their suitability for applications in s...
The assembly joints of modem solid rocket motor cases are generally sealed using conventional O-ring...
Design criteria for zero-leakage connectors for launch vehicles - plastic flow & flange rollin
Mathematical model of interface sealing phenomenon in determining design criteria for zero leakage c...
Principles of connector testing, design evaluation of commercial connectors, and assessment of desig...
Extremely fine finished surfaces as mating parts for sealing in fluid connectors and statistical ana...
Aerospace technology and design considerations for leak-tight separable, semipermanent, and permanen...
Flow control of cryogenic liquids is achieved through use of an electrical feed-through connector wi...
U-tube containing liquid indicates pressure differences in a leakage tester. This tube, connecting t...
Selection of materials for electrical connectors compatible with future space mission
Guide manual for aiding designers in selection of duct, tubing, and gasketing materials for space ve...
The assembly of flanges, seals, and pipes are used to carry cryogenic fluid from a storage tank to t...
An analytical method and a design procedure to develop flanged separable pipe connectors are discuss...
Three types of surface conditions (plain surface, plain surface with oxidation inhibitor, and toothe...
In Stennis Space Center's Component Test Facility, piping lines carry rocket propellants and high pr...
Polyimide second-stage rod seals were evaluated to determine their suitability for applications in s...
The assembly joints of modem solid rocket motor cases are generally sealed using conventional O-ring...