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Orbital maneuvering subsystem functional path analysis for performance monitoring fault detection and annunciation
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Keesler, E. L. |
| Copyright Year | 1974 |
| Description | The functional paths of the Orbital Maneuver Subsystem (OMS) is defined. The operational flight instrumentation required for performance monitoring, fault detection, and annunciation is described. The OMS is a pressure fed rocket engine propulsion subsystem. One complete OMS shares each of the two auxiliary propulsion subsystem pods with a reaction control subsystem. Each OMS is composed of a pressurization system, a propellant tanking system, and a gimbaled rocket engine. The design, development, and operation of the system are explained. Diagrams of the system are provided. |
| File Size | 1253174 |
| Page Count | 54 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740026212 |
| Archival Resource Key | ark:/13960/t3906wp7s |
| Language | English |
| Publisher Date | 1974-07-01 |
| Access Restriction | Open |
| Subject Keyword | Space Vehicles Spacecraft Maneuvers Fault Detection Self Maneuvering Units Systems Engineering Spacecraft Guidance Thrust Control Liquid Propellant Rocket Engines Rocket Engine Design Propulsion System Configurations 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 |
