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Magnetic bearing reaction wheel. [for spacecraft attitude control
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sabnis, A. Schmitt, F. Smith, L. |
| Copyright Year | 1976 |
| Description | The results of a program for the development, fabrication and functional test of an engineering model magnetically suspended reaction wheel are described. The reaction wheel develops an angular momentum of + or - 0.5 foot-pound-second and is intended for eventual application in the attitude control of long-life interplanetary and orbiting spacecraft. A description of the wheel design and its major performance characteristics is presented. Recommendations for flight prototype development are made. |
| File Size | 2863264 |
| Page Count | 84 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760020248 |
| Archival Resource Key | ark:/13960/t83j87x4d |
| Language | English |
| Publisher Date | 1976-02-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Reaction Wheels Induction Motors Attitude Control Bearings Redundancy Angular Momentum Interplanetary Spacecraft Spacecraft Control Reliability Engineering Models Tachometers Magnetic Suspension Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
