Analysis and Evaluation of German Attainments and Research in the Liquid Rocket Engine Field. Volume 4. Propellant Injectors
Abstract
This report on Propellant Injectors shows the interrelation of injector development to the design and performance characteristics of rocket engines. Various injector types are studied, design parameters established, and details of many leading foreign injectors summarized For a complete coverage of these subjects, it is recommended that all volumes of this series be consulted.; Utilization was made of the applicable portions of the 55,000 captured foreign documents relating to rocket engines, supplemented by interrogations of German technical personnel located in the United States.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1951
- Accession Number
- ADA800145