Analysis and Evaluation of German Attainments and Research in the Liquid Rocket Engine Field. Volume 8. Rocket Engine Control and Safety Circuits
Abstract
This report comprises the analysis of foreign liquid rocket research dealing with rocket engine controls and safety circuits. Leading examples of JATO, missile, and aircraft prime-mover rocket engines are analyzed to display the different control requirements and methods adopted to achieve the desired control and safety characteristics. The selection of examples permits a comparison of the control considerations when liquid oxygen is used and when nitric acid is used in anergole or hypergole propellant combinations. Wherever possible, the design details and operating experience are included. The approach used in the analysis is to state the design data and specifications which were to be met, and present notes on the interrelation between the control and safety components and other design factors. Each analysis is completed by summaries and evaluations, including possible application to American practice.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1951
- Accession Number
- ADA800120