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Evaluation of injector principles in a 2400-pound-thrust rocket engine using liquid oxygen and liquid ammonia
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1959 |
| Description | Injector evaluation in 2400-pound-thrust rocket engine using liquid oxygen and liquid ammonia |
| File Size | 172642770 |
| Page Count | 37 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19630004011 |
| Archival Resource Key | ark:/13960/t4cp1v05b |
| Language | English |
| Publisher Date | 1959-01-01 |
| Access Restriction | Open |
| Subject Keyword | Rocket Engine Liquid Oxygen /lox/ Liquid Ammonia Injector 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 |