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)
Communist Chinese Rocket Propulsion Technology: Compilation of Abstracts
1966
2 pages
Report
Keine Angabe
Englisch
Rocket Engines & Motors , Rocket Propellants , Rocket propulsion , China , Abstracts , Rocket motors , 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
Solid rocket propulsion technology
TIBKAT | 1993
|Selecting hydrocarbon rocket propulsion technology
NTRS | 1986
|Selecting hydrocarbon rocket propulsion technology
Elsevier | 1987
|TIBKAT | 1960
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