The Space Shuttle body flap is located beneath the main engine nozzles and is required for proper aerodynamic control during orbital descent. Routine inspection of one of four body flap actuators found one of the actuator bearings had degraded and blackened balls. A test program was initiated to demonstrate that it is acceptable to operate bearings which are degraded from operation over several flights. This test exposed the bearing to predicted flight axial loads, speeds and temperatures. Testing at 140 F has been completed, and results indicate the previously flown bearings are acceptable for up to 12 additional missions. Additional testing is underway to determine the lubricant life at various temperatures and stresses and to further und...
Test evaluation of high temperature greases and solid lubricants in thrust loaded ball bearing
Because many future spacecraft will require mechanisms to operate for long periods of time in enviro...
Results are presented from an investigation to determine the effects of fabrication-induced defects ...
The Space Shuttle body flap (BF) is located beneath the main engine nozzles and is required for prop...
A significantly deteriorated ball bearing mechanism from a body flap actuator on Space Shuttle OV-10...
This paper documents the work done on the bearing assessment program over the past two and a half ye...
A series of low speed experiments to evaluate the possible occurrence of transfer film lubrication a...
ABSTRACT A significantly deteriorated ball bearing mechanism from a body flap actuator on Space Shut...
As part of NASA s Return-To-Flight efforts, the Space Operations Program investigated the condition ...
A probabilistic analysis, using the 2-parameter Weibull-Johnson method, was performed on experimenta...
The cause, or causes, for the Space Shuttle Main Engine ball wear were unknown, however, several mec...
Because many future spacecraft or space stations will require mechanisms to operate for long periods...
The Z-2 is a candidate for NASA's next generation spacesuit, designed for a range of possible missio...
Sierra Nevada Corporations Space Systems performed bearing life testing for the Scan Mirror Motor/En...
A novel pin on disc tribometer was designed and constructed to generate a high-speed, wear coefficie...
Test evaluation of high temperature greases and solid lubricants in thrust loaded ball bearing
Because many future spacecraft will require mechanisms to operate for long periods of time in enviro...
Results are presented from an investigation to determine the effects of fabrication-induced defects ...
The Space Shuttle body flap (BF) is located beneath the main engine nozzles and is required for prop...
A significantly deteriorated ball bearing mechanism from a body flap actuator on Space Shuttle OV-10...
This paper documents the work done on the bearing assessment program over the past two and a half ye...
A series of low speed experiments to evaluate the possible occurrence of transfer film lubrication a...
ABSTRACT A significantly deteriorated ball bearing mechanism from a body flap actuator on Space Shut...
As part of NASA s Return-To-Flight efforts, the Space Operations Program investigated the condition ...
A probabilistic analysis, using the 2-parameter Weibull-Johnson method, was performed on experimenta...
The cause, or causes, for the Space Shuttle Main Engine ball wear were unknown, however, several mec...
Because many future spacecraft or space stations will require mechanisms to operate for long periods...
The Z-2 is a candidate for NASA's next generation spacesuit, designed for a range of possible missio...
Sierra Nevada Corporations Space Systems performed bearing life testing for the Scan Mirror Motor/En...
A novel pin on disc tribometer was designed and constructed to generate a high-speed, wear coefficie...
Test evaluation of high temperature greases and solid lubricants in thrust loaded ball bearing
Because many future spacecraft will require mechanisms to operate for long periods of time in enviro...
Results are presented from an investigation to determine the effects of fabrication-induced defects ...