COMMUNIST CHINESE ROCKET PROPULSION TECHNOLOGY: COMPILATION OF ABSTRACTS.
LIBRARY OF CONGRESS WASHINGTON D C AEROSPACE TECHNOLOGY DIV
Pagination or Media Count:
This compilation of abstracts is based on CHICOM open sources published 1960-1966. It consists of 31 abstracts dealing with solid and liquid rocket propulsion technology. The abstracts are arranged alphabetically by author. Pertinent information included shock-wave tube, thrust vector control and secondary injection for solid-propellant rockets, rocket materials body and engine materials, chemical problems in combustion and flame, problems of rocket propellant chemistry, stress analysis of cast solid rocket grains, pyrometers, heat transfer in turbojet combustion chambers, film cooling effects, supersonic flow of nonequilibrium dissociating gas passing through a circular cone at an incidence angle, mathematical principles for rocket flights. Author
- Rocket Engines
- Rocket Propellants