Accession Number:

AD0641892

Title:

COMMUNIST CHINESE ROCKET PROPULSION TECHNOLOGY: COMPILATION OF ABSTRACTS.

Descriptive Note:

Corporate Author:

LIBRARY OF CONGRESS WASHINGTON D C AEROSPACE TECHNOLOGY DIV

Personal Author(s):

Report Date:

1966-07-11

Pagination or Media Count:

29.0

Abstract:

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

Descriptors:

• (*ROCKET PROPULSION
• CHINA)
• ABSTRACTS
• ROCKET ENGINES
• SHOCK WAVES
• THRUST VECTOR CONTROL SYSTEMS
• COMBUSTION
• FLAME PROPAGATION
• SOLID ROCKET PROPELLANTS
• LIQUID ROCKET PROPELLANTS
• ROCKET PROPELLANT GRAINS
• PYROMETERS
• FILM COOLING
• COMBUSTION CHAMBERS
• SUPERSONIC FLOW
• HEAT RESISTANT MATERIALS
• TRAJECTORIES

Subject Categories:

• Rocket Engines
• Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE