Add to ORKGDesign criteria for zero-leakage connectors for launch vehicles - plastic flow & flange rollin
Selection of materials for electrical connectors compatible with future space mission
The development of and operational programs for effective use in design are presented for liquid roc...
An analysis and design effort directed to advancing the state-of-the-art of space storable isolation...
Mathematical model of interface sealing phenomenon in determining design criteria for zero leakage c...
Pressure pulses, shock and vibratory loading on launch vehicle connectors - heat environment, vacuum...
Extremely fine finished surfaces as mating parts for sealing in fluid connectors and statistical ana...
Principles of connector testing, design evaluation of commercial connectors, and assessment of desig...
An analytical method and a design procedure to develop flanged separable pipe connectors are discuss...
A study program has been conducted to explore new methods of achieving zero leakage, separable and s...
Aerospace technology and design considerations for leak-tight separable, semipermanent, and permanen...
Guide manual for aiding designers in selection of duct, tubing, and gasketing materials for space ve...
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...
State of the art and design criteria for components used in liquid propellant rocket propulsion syst...
The assembly of flanges, seals, and pipes are used to carry cryogenic fluid from a storage tank to t...
Selection of materials for electrical connectors compatible with future space mission
The development of and operational programs for effective use in design are presented for liquid roc...
An analysis and design effort directed to advancing the state-of-the-art of space storable isolation...
Mathematical model of interface sealing phenomenon in determining design criteria for zero leakage c...
Pressure pulses, shock and vibratory loading on launch vehicle connectors - heat environment, vacuum...
Extremely fine finished surfaces as mating parts for sealing in fluid connectors and statistical ana...
Principles of connector testing, design evaluation of commercial connectors, and assessment of desig...
An analytical method and a design procedure to develop flanged separable pipe connectors are discuss...
A study program has been conducted to explore new methods of achieving zero leakage, separable and s...
Aerospace technology and design considerations for leak-tight separable, semipermanent, and permanen...
Guide manual for aiding designers in selection of duct, tubing, and gasketing materials for space ve...
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...
State of the art and design criteria for components used in liquid propellant rocket propulsion syst...
The assembly of flanges, seals, and pipes are used to carry cryogenic fluid from a storage tank to t...
Selection of materials for electrical connectors compatible with future space mission
The development of and operational programs for effective use in design are presented for liquid roc...
An analysis and design effort directed to advancing the state-of-the-art of space storable isolation...