The increased thrust, higher engine performance, and greater reliability requirements of the Titan IIIM engines for application to the Manned Orbital Laboratory Program necessitated extensive redesign of the thrust chamber assembly as well as other major components for the Stage I engine. The report encompasses the design and development of the combustion chamber. (Author)
Program Titan IIIM Standard Space Launch Vehicle Component Development Report for the Titan IIIM Stage I Combustion Chamber
1969
235 pages
Report
Keine Angabe
Englisch
Combustion & Ignition , Space Launch Vehicles & Support Equipment , Manned Spacecraft , Manned spacecraft , Space stations , Combustion chambers , Launch vehicles , Design , Space capsules , Alloys , Manufacturing , Heat transfer , Stresses , Fuel injection , Propellant control , Structural properties , Gemini b project , Manned orbital laboratories , Gemini , Nickel alloy hastelloy alloy x , Titan 3
Titan Launch Vehicle Program overview
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