Experimental vibration characteristics of a 1/40-scale dynamic model of the Saturn 5 launch umbilical tower configuration
Vibration characteristics of 1/40 scale model of Saturn 5 launch vehicle and umbilical tower configuration
Catherines, J. J.↗
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Vibration analysis of a 1/40-scale dynamic model of Saturn 5 launch platform-umbilical tower configuration
Direct stiffness method of computing vibrational characteristics of dynamic model of Apollo- Saturn 5 vehicle - umbilical tower configuration
Adelman, H. M.↗
Saturn 5 launcher-umbilical tower vibration analysis. Volume 2 - A computer program for analysis of the vibrational characteristics of large linear space frames Final report
Computer program for analyzing vibrational characteristics of Saturn 5 launcher-umbilical tower complex
Source record↗
Saturn 5-Launcher-Umbilical tower vibration analysis. Volume 1 - Response to ground wind excitation Final report
Saturn 5 umbilical tower vibration analysis due to ground wind excitation
Jones, C. E.↗
Vacuum jacketed umbilical lines technology advancement study. Task 1 - Burst discs, task 1 Final technical report
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - burst discs
Martinez, J.↗
Vacuum jacketed umbilical lines technology advancement study. Task 2 - Vacuum seal valves Final technical report
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - vacuum seal valves
Martinez, J.↗
Vacuum jacketed umbilical lines technology advancement study. Task 3, sub-task 1 - vacuum jacketed hose flexure Final technical report
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - hose flexure lines
Kimble, K.↗
Vacuum jacketed umbilical lines technology advancement study. Task 3, sub-task 2 - Vacuum and CO2 jacketed line repair techniques Final technical report
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - repair techniques for carbon dioxide and vacuum jacketed transfer lines
Kimble, K.↗
Vacuum jacketed umbilical lines technology advancement study. Task 4 - Rotary joint Final technical report
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - low heat cryogenic rotary joint
Mursinna, R. C.↗
Vacuum jacketed umbilical lines technology advancement study. Task 5 - Vacuum probes Final technical report
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - vacuum probes
Rewerts, G. R.↗
Vacuum jacketed umbilical lines technology advancement study. Task 6 - Central vacuum pulldown system Final technical report
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - central vacuum pulldown system
Rewerts, G. R.↗
Vacuum jacketed umbilical lines technology advancement study. Task 7 - Bayonet joint Final technical report
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - bayonet joints in cryogenic propellant and vent lines
Mursinna, R. C.↗
Umbilical disconnect Patent
Remotely actuated quick disconnect mechanism for umbilical cables
Clickner, R. E., Jr.↗
Research and development of umbilical hose assembly concepts for manned space flight including design verification test report REDAR-RTR-351
Umbilical hose assembly and PLSS oxygen and water hose designs
Sylvester, W. A.↗
Final configuration selected for the umbilical hose assembly and LCG water system
Design verification test results for umbilical hose and PLSS water and oxygen hoses
Fox, L. C.↗
Power system interface and umbilical system study
System requirements and basic design criteria were defined for berthing or docking a payload to the 25 kW power module which will provide electrical power and attitude control, cooling, data transfer, and communication services to free-flying and Orbiter sortie payloads. The selected umbilical system concept consists of four assemblies and command and display equipment to be installed at the Orbiter payload specialist station: (1) a movable platen assembly which is attached to the power system with EVA operable devices; (2) a slave platen assembly which is attached to the payload with EVA operable devices; (3) a fixed secondary platen permanently installed in the power system; and (4) a fixed secondary platen permanently installed on the payload. Operating modes and sequences are described.
Source record↗
Optical data transmission technology for fixed and drag-on STS payload umbilicals, volume 2
Optical data handling methods are studied as applicable to payload communications checkout and monitoring. Both payload umbilicals and interconnecting communication lines carrying payload data are examined for the following: (1) ground checkout requirements; (2) optical approach (technical survey of optical approaches, selection of optimum approach); (3) survey and select components; (4) compare with conventional approach; and (5) definition of follow on activity.
St.denis, R. W.↗