30th Aerospace Mechanisms SymposiumThe proceedings of the 30th Aerospace Mechanisms Symposium are reported. NASA Langley Research Center hosted the proceedings held at the Radisson Hotel in Hampton, Virginia on May 15-17, 1996, and Lockheed Martin Missiles and Space Company, Inc. co-sponsored the symposium. Technological areas covered include bearings and tribology; pointing, solar array, and deployment mechanisms; orbiter/space station; and other mechanisms for spacecraft.
Document ID
19960025595
Acquisition Source
Langley Research Center
Document Type
Conference Proceedings
Authors
Bradley, Obie H., Jr. (NASA Langley Research Center Hampton, VA United States)
Rogers, John F. (NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 17, 2013
Publication Date
May 1, 1996
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-CP-3328NAS 1.55:3328L-17569Report Number: NASA-CP-3328Report Number: NAS 1.55:3328Report Number: L-17569
IDRelationTitle19960025603WorkA Nitinol-Based Solar Array Deployment Mechanism19960025615WorkDevelopment of a hermetically sealed brushless DC motor for a J-T cryocooler19960025597WorkSpace Telescope Fine Guidance Sensor Bearing Anomaly19960025600WorkNew Antenna Deployment, Pointing and Supporting Mechanism19960025614WorkReliability and testing19960025624WorkThe micro conical system: Lessons learned from a successful EVA/robot-compatible mechanism19960025599WorkTape recorder failure investigation19960025610WorkAdvances in the analysis and design of constant-torque springs19960025623WorkMagnetic docking aid for orbiter to ISS docking19960025609WorkDesign and development of the Cassini main engine assembly Gimbal mechanism19960025618WorkRemote manual operator for space station intermodule ventilation valve19960025619WorkMiniature rotary actuator19960025607WorkAntenna pointing mechanism for ESA ENVISAT polar platform19960025613WorkMars pathfinder lander deployment mechanisms19960025620WorkMir environmental effects payload handrail clamp/pointing device19960025605WorkSCARLET I: Mechanization solutions for deployable concentrator optics integrated with rigid array technology19960025596WorkLife test results for the advanced very high resolution radiometer scanner19960025621WorkA computer controlled power tool for the servicing of the Hubble Space Telescope19960025617WorkEVA assembly and release of highly loaded bolts19960025611WorkJettison system for a large inflatable antenna19960025598WorkThe thermal conductance of solid-lubricated bearings at cryogenic temperatures in vacuum19960025612WorkMars pathfinder Rover egress deployable ramp assembly19960025608WorkDevelopment of a Gimballed, dual frequency, space-based, microwave antenna for volume production19960025625WorkNASA space shuttle lightweight seat19960025622WorkUmbilical mechanism assembly for the international space station19960025602WorkCoarse pointing mechanism assembly for satellite interlink experiment19960025606WorkA revolute joint with linear load-displacement response for a deployable lidar telescope19960025601WorkDevelopment of a scan mirror assembly for an extreme ultraviolet atmospheric scanner19960025604WorkThe ARA Mark 3 solar array design and development19960025616WorkThe design, development and qualification of a lightweight antenna pointing mechanism19960025596WorkLife test results for the advanced very high resolution radiometer scanner19960025597WorkSpace Telescope Fine Guidance Sensor Bearing Anomaly19960025598WorkThe thermal conductance of solid-lubricated bearings at cryogenic temperatures in vacuum19960025599WorkTape recorder failure investigation19960025600WorkNew Antenna Deployment, Pointing and Supporting Mechanism19960025601WorkDevelopment of a scan mirror assembly for an extreme ultraviolet atmospheric scanner19960025602WorkCoarse pointing mechanism assembly for satellite interlink experiment19960025603WorkA Nitinol-Based Solar Array Deployment Mechanism19960025604WorkThe ARA Mark 3 solar array design and development19960025605WorkSCARLET I: Mechanization solutions for deployable concentrator optics integrated with rigid array technology19960025606WorkA revolute joint with linear load-displacement response for a deployable lidar telescope19960025607WorkAntenna pointing mechanism for ESA ENVISAT polar platform19960025608WorkDevelopment of a Gimballed, dual frequency, space-based, microwave antenna for volume production19960025609WorkDesign and development of the Cassini main engine assembly Gimbal mechanism19960025610WorkAdvances in the analysis and design of constant-torque springs19960025611WorkJettison system for a large inflatable antenna19960025612WorkMars pathfinder Rover egress deployable ramp assembly19960025613WorkMars pathfinder lander deployment mechanisms19960025614WorkReliability and testing19960025615WorkDevelopment of a hermetically sealed brushless DC motor for a J-T cryocooler19960025616WorkThe design, development and qualification of a lightweight antenna pointing mechanism19960025617WorkEVA assembly and release of highly loaded bolts19960025618WorkRemote manual operator for space station intermodule ventilation valve19960025619WorkMiniature rotary actuator19960025620WorkMir environmental effects payload handrail clamp/pointing device19960025621WorkA computer controlled power tool for the servicing of the Hubble Space Telescope19960025622WorkUmbilical mechanism assembly for the international space station19960025623WorkMagnetic docking aid for orbiter to ISS docking19960025624WorkThe micro conical system: Lessons learned from a successful EVA/robot-compatible mechanism19960025625WorkNASA space shuttle lightweight seat