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Pressure fed thrust chamber technology program (Document No: 19920022306)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Dunn, Glen M. |
| Copyright Year | 1992 |
| Description | This is the final report for the Pressure Fed Technology Program. It details the design, fabrication, and testing of subscale hardware which successfully characterized Liquid Oxygen Rocket Propulsion (LOX/RP) combustion for low cost pressure fed design. The innovative modular injector design is described in detail as well as hot-fire test results which showed excellent performance. The program summary identifies critical LOX/RP design issues that have been resolved in this testing, and details the low risk development requirements for low cost engines for future Expandable Launch Vehicles (ELV). |
| File Size | 21364699 |
| Page Count | 126 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19920022306 |
| Archival Resource Key | ark:/13960/t2r54jk52 |
| Language | English |
| Publisher Date | 1992-07-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Fabrication Performance Tests Pressure Effects Injectors Launch Vehicles Low Cost Liquid Oxygen Technology Assessment Thrust Chambers Liquid Propellant Rocket Engines 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 |
