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Predicted performance of an integrated modular engine system
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Felder, James L. Binder, Michael |
| Copyright Year | 1993 |
| Description | Space vehicle propulsion systems are traditionally comprised of a cluster of discrete engines, each with its own set of turbopumps, valves, and a thrust chamber. The Integrated Modular Engine (IME) concept proposes a vehicle propulsion system comprised of multiple turbopumps, valves, and thrust chambers which are all interconnected. The IME concept has potential advantages in fault-tolerance, weight, and operational efficiency compared with the traditional clustered engine configuration. The purpose of this study is to examine the steady-state performance of an IME system with various components removed to simulate fault conditions. An IME configuration for a hydrogen/oxygen expander cycle propulsion system with four sets of turbopumps and eight thrust chambers has been modeled using the Rocket Engine Transient Simulator (ROCETS) program. The nominal steady-state performance is simulated, as well as turbopump thrust chamber and duct failures. The impact of component failures on system performance is discussed in the context of the system's fault tolerant capabilities. |
| File Size | 1015387 |
| Page Count | 22 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19950017371 |
| Archival Resource Key | ark:/13960/t6935rj0f |
| Language | English |
| Publisher Date | 1993-07-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Propulsion System Performance Performance Prediction Valves Computerized Simulation Modularity Propulsion System Configurations Spacecraft Propulsion Fault Tolerance Turbine Pumps Spacecraft Reliability Thrust Chambers Hydrogen Oxygen Engines Rocket Engine Design Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |