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Space shuttle engineering and operations support. orbiter to spacelab electrical power interface. avionics system engineering
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Emmons, T. E. |
| Copyright Year | 1976 |
| Description | The results are presented of an investigation of the factors which affect the determination of Spacelab (S/L) minimum interface main dc voltage and available power from the orbiter. The dedicated fuel cell mode of powering the S/L is examined along with the minimum S/L interface voltage and available power using the predicted fuel cell power plant performance curves. The values obtained are slightly lower than current estimates and represent a more marginal operating condition than previously estimated. |
| File Size | 2742741 |
| Page Count | 30 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760021252 |
| Archival Resource Key | ark:/13960/t9d55dv6p |
| Language | English |
| Publisher Date | 1976-06-30 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Interfaces Operations Research Spacelab Systems Engineering Fuel Cells Space Shuttles Spacecraft Power Supplies Space Shuttle Orbiters Avionics 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 |
