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Iue/ira system description
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Jennings, J. |
| Copyright Year | 1977 |
| Description | The IUE/IRA rate sensor system designed to meet the requirements of the International Ultraviolet Explorer spacecraft mission is described. The system consists of the sensor unit containing six rate sensor modules and the electronic control unit containing the rate sensor support electronics and the command/control circuitry. The inertial reference assembly formed by the combined units will provide spacecraft rate information for use in the stabilization and control system. The system is described in terms of functional description, operation redundancy performance, mechanical interface, and electrical interface. Test data obtained from the flight unit are summarized. |
| File Size | 40245826 |
| Page Count | 109 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810012586 |
| Archival Resource Key | ark:/13960/t9s22s41n |
| Language | English |
| Publisher Date | 1977-09-08 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Spacecraft Instruments Inertial Reference Systems Iue Spacecraft Control Spacecraft Stability Gyroscopes Spacecraft Electronic Equipment 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 |
