Add to ORKGThis paper presents the design and developmental testing associated with the bearing, motor, and roll ring module (BMRRM) used for the beta rotation axis on International Space Station Alpha (ISSA). The BMRRM with its controllers located in the electronic control unit (ECU), provides for the solar array pointing and tracking functions as well as power and signal transfer across a rotating interface
The photovoltaic solar panels on the International Space Station (ISS) track the Sun through continu...
The design and development of a dry lubricated direct solar array pointing mechanism is discussed fr...
The Parabolic Offset Linearly Actuated Reflector (POLAR) solar dynamic module was selected as the ba...
Perhaps the most critical structural system aboard the Space Station is the Solar Alpha Rotary Joint...
Electrical power, command signals and data are transferred across the Space Station Freedom solar al...
The Solar Alpha Rotary Joint (SARJ) is a single-axis pointing mechanism used to orient the solar pow...
The ISS utilizes two large rotating mechanisms, the SARJ, as part of the solar arrays alignment syst...
The most critical mechanism on board the proposed space station is the continously rotating joint wh...
The SARJ LITE (Lubrication Interval Test) test rig was built as a method to evaluate the performance...
The International Space Station (ISS) is the largest and most complex spacecraft ever assembled and ...
The application of a Bearing and Power Transfer Assembly (BAPTA) to a Solar Array Drive for communic...
The space station uses precision rotary gimbals to provide for sun tracking of its photoelectric arr...
This paper describes the development of an ETU (Engineering Test Unit) rotary optical chopper with m...
The International Space Station (ISS) is the largest and most complex spacecraft ever assembled and ...
Launched June 18, 2009 on an Atlas V rocket, NASA's Lunar Reconnaissance Orbiter (LRO) is the first ...
The photovoltaic solar panels on the International Space Station (ISS) track the Sun through continu...
The design and development of a dry lubricated direct solar array pointing mechanism is discussed fr...
The Parabolic Offset Linearly Actuated Reflector (POLAR) solar dynamic module was selected as the ba...
Perhaps the most critical structural system aboard the Space Station is the Solar Alpha Rotary Joint...
Electrical power, command signals and data are transferred across the Space Station Freedom solar al...
The Solar Alpha Rotary Joint (SARJ) is a single-axis pointing mechanism used to orient the solar pow...
The ISS utilizes two large rotating mechanisms, the SARJ, as part of the solar arrays alignment syst...
The most critical mechanism on board the proposed space station is the continously rotating joint wh...
The SARJ LITE (Lubrication Interval Test) test rig was built as a method to evaluate the performance...
The International Space Station (ISS) is the largest and most complex spacecraft ever assembled and ...
The application of a Bearing and Power Transfer Assembly (BAPTA) to a Solar Array Drive for communic...
The space station uses precision rotary gimbals to provide for sun tracking of its photoelectric arr...
This paper describes the development of an ETU (Engineering Test Unit) rotary optical chopper with m...
The International Space Station (ISS) is the largest and most complex spacecraft ever assembled and ...
Launched June 18, 2009 on an Atlas V rocket, NASA's Lunar Reconnaissance Orbiter (LRO) is the first ...
The photovoltaic solar panels on the International Space Station (ISS) track the Sun through continu...
The design and development of a dry lubricated direct solar array pointing mechanism is discussed fr...
The Parabolic Offset Linearly Actuated Reflector (POLAR) solar dynamic module was selected as the ba...