DYNAMIC PROCESSES IN A LIQUID PROPELLANT ROCKET ENGINE (CHAPTER III),
Abstract
Contents: Characteristic designs of engines and possible variants of the sequence of their operation; Character of relation between parameters of chamber and parameters of circuits; Investigation of relation between averaged parameters and dynamic processes by method of small finite deviations; Use of computer techniques in the investigation of rocket engines.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 16, 1965
- Accession Number
- AD0622607
Entities
People
- E. K. Moshkin
Organizations
- National Air and Space Intelligence Center