Analysis and Evaluation of German Attainments and Research in the Liquid Rocket Engine Field. Volume 7. Thrust Control
Abstract
This volume on Thrust Control makes an analysis of the various thrust-control systems utilized on both gas-pressure and pump-pressure feed systems and presents detailed analysis, showing both the degree of complication and simplicity which can be achieved depending upon the requirements established for the use of the rocket engine. 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
- Jan 01, 1951
- Accession Number
- ADA800132