Add to ORKGThe reduction of residual unbalance in the space shuttle main engine (SSME) high pressure turbopump rotors was addressed. Elastic rotor response to unbalance and balancing requirements, multiplane and in housing balancing, and balance related rotor design considerations were assessed. Recommendations are made for near term improvement of the SSME balancing and for future study and development efforts
Vibration generated from main rotor unbalance has a major impact on the aerospace gas turbine indust...
In response to a request from the House of Representatives Committee on Science, Space, and Technolo...
Rotordynamical analyses are typically performed using rigid disk models. Studies of rotor models in ...
Transient unbalance shifts were determined not to excite a rotor instability in the high pressure tu...
LectureThe paper describes elastic balancing procedures and experimental results for turbomachine ro...
An unbalance is the most common issue affecting the turbomachinery rotors. A machine operation at hi...
The SSME when developed in the 1970's was a technological leap in space launch propulsion system des...
A review is presented of various rotordynamic problems which have been encountered and eliminated in...
Rotational stability of turbopump components in the space shuttle main engine was studied via analys...
Rotary dynamics test facility investigates and corrects imbalances in rotary components at speeds up...
The operating requirements established by NASA for the SSME were considerably more demanding than th...
The Space Shuttle Main Engine (SSME) is a reusable, high performance rocket engine being developed t...
International Telemetering Conference Proceedings / October 24-27, 1983 / Sheraton-Harbor Island Hot...
The main engines for the Future Shuttle will focus on improved safety and operability. Performance e...
Through the years of the Space Shuttle Main Engine (SSME) program the engine has evolved and operati...
Vibration generated from main rotor unbalance has a major impact on the aerospace gas turbine indust...
In response to a request from the House of Representatives Committee on Science, Space, and Technolo...
Rotordynamical analyses are typically performed using rigid disk models. Studies of rotor models in ...
Transient unbalance shifts were determined not to excite a rotor instability in the high pressure tu...
LectureThe paper describes elastic balancing procedures and experimental results for turbomachine ro...
An unbalance is the most common issue affecting the turbomachinery rotors. A machine operation at hi...
The SSME when developed in the 1970's was a technological leap in space launch propulsion system des...
A review is presented of various rotordynamic problems which have been encountered and eliminated in...
Rotational stability of turbopump components in the space shuttle main engine was studied via analys...
Rotary dynamics test facility investigates and corrects imbalances in rotary components at speeds up...
The operating requirements established by NASA for the SSME were considerably more demanding than th...
The Space Shuttle Main Engine (SSME) is a reusable, high performance rocket engine being developed t...
International Telemetering Conference Proceedings / October 24-27, 1983 / Sheraton-Harbor Island Hot...
The main engines for the Future Shuttle will focus on improved safety and operability. Performance e...
Through the years of the Space Shuttle Main Engine (SSME) program the engine has evolved and operati...
Vibration generated from main rotor unbalance has a major impact on the aerospace gas turbine indust...
In response to a request from the House of Representatives Committee on Science, Space, and Technolo...
Rotordynamical analyses are typically performed using rigid disk models. Studies of rotor models in ...