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Space transportation booster engine thrust chamber technology, large scale injector
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Schneider, J. A. |
| Copyright Year | 1993 |
| Description | The objective of the Large Scale Injector (LSI) program was to deliver a 21 inch diameter, 600,000 lbf thrust class injector to NASA/MSFC for hot fire testing. The hot fire test program would demonstrate the feasibility and integrity of the full scale injector, including combustion stability, chamber wall compatibility (thermal management), and injector performance. The 21 inch diameter injector was delivered in September of 1991. |
| File Size | 101251411 |
| Page Count | 456 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930017368 |
| Archival Resource Key | ark:/13960/t8z94578c |
| Language | English |
| Publisher Date | 1993-02-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Space Transportation Test Stands Combustion Stability Liquid Oxygen Thrust Chambers Temperature Control Fuel Injection Booster Rocket Engines 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 |
