| Title: | A high-performance 250-pound-thrust rocket engine utilizing coaxial-flow injection of JP-4 fuel and liquid oxygen |
| Author: | Stein, Samuel |
| Author: | Langley Research Center |
| Note: | National Aeronautics and Space Administration, 1959 |
| Link: | page images at HathiTrust |
| No stable link: | This is an uncurated book entry from our extended bookshelves, readable online now but without a stable link here. You should not bookmark this page, but you can request that we add this book to our curated collection, which has stable links. |
| Subject: | Annular flow |
| Subject: | Coaxial flow |
| Subject: | Fuel injection |
| Subject: | Injectors |
| Subject: | JP-4 jet fuel |
| Subject: | Liquid atomization |
| Subject: | Liquid oxygen |
| Subject: | Propulsive efficiency |
| Subject: | Rocket engine design |
| Subject: | Rocket engines |
| Subject: | Rocket thrust |
| Subject: | Wind tunnel models |
| Other copies: | Look for editions of this book at your library, or elsewhere. |
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