"Development of LOX/RP-1 Engines for Saturn/Apollo Launch Vehicles."
The development of liquid rocket engines follow similar patterns regardless of engine size. During the development of the H-1 and F-1 engines, many problems were encountered. Methods of solving the combustion instability problem are discussed. A description is given of the major components of eac...
| Main Author: | |
|---|---|
| Format: | Electronic |
| Published: |
University of Alabama in Huntsville Archives
|
| Subjects: | |
| Online Access: | http://libarchstor2.uah.edu/digitalcollections/items/show/11056 |